National Library of Energy BETA

Sample records for median aerodynamic diameter

  1. Characterization of an aerodynamic lens for transmitting particles greater than 1 micrometer in diameter into the Aerodyne aerosol mass spectrometer

    E-Print Network [OSTI]

    Williams, L. R.

    We have designed and characterized a new inlet and aerodynamic lens for the Aerodyne aerosol mass spectrometer (AMS) that transmits particles between 80 nm and more than 3 ?m in vacuum aerodynamic diameter. The design of ...

  2. Aerodynamic Performance of a 5-Metre-Diameter Darrieus Turbine With Extruded

    E-Print Network [OSTI]

    -diameter vertical-axis wind turbine has undergone continued testing since 1976 at the Sandia Laboratories Wind Division 4715. #12;CONTENTS NOMENCLATURE SUMMARY Introduction The 5-Metre Vertical-Axis Wind Turbine ILLUSTRATIONS The 5-Metre Vertical-Axis Wind Turbine at Sandia Labora- tories Test Site Original Three

  3. Sandia Energy - Rotor Aerodynamic Design

    Broader source: All U.S. Department of Energy (DOE) Office Webpages (Extended Search)

    Aerodynamic Design Home Stationary Power Energy Conversion Efficiency Wind Energy Rotor Innovation Rotor Aerodynamic Design Rotor Aerodynamic DesignTara Camacho-Lopez2015-05-28T16:...

  4. Integer-Sided Triangles with integral medians

    E-Print Network [OSTI]

    Konstantine Zelator

    2013-08-15

    In this work, we prove that any triangle whose three sidelengths are integers, cannot have all of its three medians also having integral lengths.This is done in Proposition 2.In Section 5, we give precise(i.e.necessary and sufficient)conditions for a nonisosceles, integer-sided triangle to have two integral medians.In Section 3, we offer parametric descriptions of three special families of integer-sided triangles.The first family consists of all Pythagorean triangles whose medians to their hypotenuses is integral. The other two medians (to the two legs)of any Pythagorean triangle are irrational, a proof of this fact can be found in reference 4 of this paper.The second family consists of all integer-sided isosceles triangles, whose only integral median is the one contained between the two sides of equal length. Finally, the third family consists of all isosceles integer-sided triangles with the two medians of equal length;having integer length.

  5. Theoretical advances on multichromosomal median computation

    E-Print Network [OSTI]

    Chauve, Cedric

    consider the classical problem of com- puting an optimal median for three multichromosomal genomes G1, G2, G3. More precisely, we consider the case where ­ G1, G2, G3 are mixed genomes as they can have (possibly) both linear and circular chromosomes; ­ pairs G, G of genomes on n genes are compared using

  6. Computational Aerodynamics and Aeroacoustics for Wind Turbines

    E-Print Network [OSTI]

    Computational Aerodynamics and Aeroacoustics for Wind Turbines #12;#12;Computational Aerodynamics and Aeroacoustics for Wind Turbines Wen Zhong Shen Fluid Mechanics Department of Mechanical Engineering TECHNICAL Shen, Wen Zhong Computational Aerodynamics and Aeroacoustics for Wind Turbines Doctor Thesis Technical

  7. Freight Wing Trailer Aerodynamics

    SciTech Connect (OSTI)

    Graham, Sean (Primary Investigator); Bigatel, Patrick

    2004-10-17

    Freight Wing Incorporated utilized the opportunity presented by this DOE category one Inventions and Innovations grant to successfully research, develop, test, patent, market, and sell innovative fuel and emissions saving aerodynamic attachments for the trucking industry. A great deal of past scientific research has demonstrated that streamlining box shaped semi-trailers can significantly reduce a truck's fuel consumption. However, significant design challenges have prevented past concepts from meeting industry needs. Market research early in this project revealed the demands of truck fleet operators regarding aerodynamic attachments. Products must not only save fuel, but cannot interfere with the operation of the truck, require significant maintenance, add significant weight, and must be extremely durable. Furthermore, SAE/TMC J1321 tests performed by a respected independent laboratory are necessary for large fleets to even consider purchase. Freight Wing used this information to create a system of three practical aerodynamic attachments for the front, rear and undercarriage of standard semi trailers. SAE/TMC J1321 Type II tests preformed by the Transportation Research Center (TRC) demonstrated a 7% improvement to fuel economy with all three products. If Freight Wing is successful in its continued efforts to gain market penetration, the energy and environmental savings would be considerable. Each truck outfitted saves approximately 1,100 gallons of fuel every 100,000 miles, which prevents over 12 tons of CO2 from entering the atmosphere. If all applicable trailers used the technology, the country could save approximately 1.8 billion gallons of diesel fuel, 18 million tons of emissions and 3.6 billion dollars annually.

  8. Integrated External Aerodynamic and Underhood Thermal Analysis...

    Office of Energy Efficiency and Renewable Energy (EERE) Indexed Site

    External Aerodynamic and Underhood Thermal Analysis for Heavy Vehicles Integrated External Aerodynamic and Underhood Thermal Analysis for Heavy Vehicles 2012 DOE Hydrogen and Fuel...

  9. Aerodynamic characteristics of seven symmetrical airfoil sections...

    Office of Scientific and Technical Information (OSTI)

    180-degree angle of attack for use in aerodynamic analysis of vertical axis wind turbines Citation Details In-Document Search Title: Aerodynamic characteristics of seven...

  10. Double diameter boring tool

    DOE Patents [OSTI]

    Ashbaugh, F.A.; Murry, K.R.

    1986-02-10

    A boring tool and a method of operation are provided for boring two concentric holes of precision diameters and depths in a single operation. The boring tool includes an elongated tool body, a shank for attachment to a standard adjustable boring head which is used on a manual or numerical control milling machine and first and second diametrically opposed cutting flutes formed for cutting in opposite directions. The diameter of the elongated tool body is substantially equal to the distance from the first flute tip to the axis of rotation plus the distance from the second flute tip to the axis of rotation. The axis of rotation of the tool is spaced from the tool centerline a distance substantially equal to one-half the distance from the second flute tip to the axis of rotation minus one-half the distance from the first flute tip to the axis of rotation. The method includes the step of inserting the boring tool into the boring head, adjusting the distance between the tool centerline and the tool axis of rotation as described above and boring the two concentric holes.

  11. Double diameter boring tool

    DOE Patents [OSTI]

    Ashbaugh, Fred N. (Belton, MO); Murry, Kenneth R. (Odessa, MO)

    1988-12-27

    A boring tool and a method of operation are provided for boring two concentric holes of precision diameters and depths in a single operation. The boring tool includes an elongated tool body, a shank for attachment to a standard adjustable boring head which is used on a manual or numerical control milling machine and first and second diametrically opposed cutting edges formed for cutting in opposite directions. The diameter of the elongated tool body is substantially equal to the distance from the first cutting edge tip to the axis of rotation plus the distance from the second cutting edge tip to the axis of rotation. The axis of rotation of the tool is spaced from the tool centerline a distance substantially equal to one-half the distance from the second cutting edge tip to the axis of rotation minus one-half the distance from the first cutting edge tip to the axis of rotation. The method includes the step of inserting the boring tool into the boring head, adjusting the distance between the tool centerline and the tool axis of rotation as described above and boring the two concentric holes.

  12. CFD-based Optimization for Automotive Aerodynamics

    E-Print Network [OSTI]

    Dumas, Laurent

    Chapter 1 CFD-based Optimization for Automotive Aerodynamics Laurent Dumas Abstract The car drag- ments. An overview of the main characteristics of automotive aerodynamics and a detailed presentation.dumas@upmc.fr) 1 #12;2 Laurent Dumas 1.1 Introducing Automotive Aerodynamics 1.1.1 A Major Concern for Car

  13. TIMEINTEGRATION METHODS IN COMPUTATIONAL AERODYNAMICS

    E-Print Network [OSTI]

    Stanford University

    flow & % #12;' $ Aerodynamic Flow computations AIRPLANE DENSITY from 0.6250 to 1.1000 AIRPLANE CP from AIRPLANE DENSITY from 0.6250 to 1.1000 AIRPLANE DENSITY from 0.0000 to 2.0000 Density contours for transonic and supersonic flow over the MD-11 and Hermes Space Shuttle & % #12;' $ Mach Number Contours

  14. Reactive Stochastic Local Search Algorithms for the Genomic Median Problem

    E-Print Network [OSTI]

    Wolf, Christian

    Reactive Stochastic Local Search Algorithms for the Genomic Median Problem Renaud Lenne1 5558, Universit´e de Lyon 1, France eric.tannier@inria.fr Abstract. The genomic median problem of the common ancestor to multiple living species. It is formulated as the search for a genome that minimizes

  15. Introduction The median problem for the reversal distance in

    E-Print Network [OSTI]

    Lonardi, Stefano

    genomes E. Ohlebusch, M.I. Abouelhoda, K. Hockel, J. Stallkamp University of Ulm, Germany CPM 2005 The median problem for the reversal distance in circular bacterial genomes #12;Introduction Methods Conclusion General Problem Distances Specific Problem Median Problem Given 3 genomes G1, G2, and G3, find

  16. Aerodynamic characteristics of seven symmetrical airfoil sections...

    Office of Scientific and Technical Information (OSTI)

    axis wind turbines Sheldahl, R E; Klimas, P C 17 WIND ENERGY; DARRIEUS ROTORS; TURBINE BLADES; AERODYNAMICS; AIRFOILS; COMPARATIVE EVALUATIONS; DATA COMPILATION;...

  17. Placement of Traffic Barriers on Roadside and Median Slopes

    E-Print Network [OSTI]

    Ferdous, Md Rubiat

    2011-08-08

    terrains are investigated using numerical simulations. A procedure is developed that provide guidance for their placement on roadside and median slopes. The research approach consists of nonlinear finite element analyses and multi-rigid-body dynamic...

  18. NMDOT Application for Permit to Construct an Access or Median...

    Open Energy Info (EERE)

    NMDOT Application for Permit to Construct an Access or Median Opening on Public Right of Way Jump to: navigation, search OpenEI Reference LibraryAdd to library Legal Document-...

  19. AERODYNAMIC AND ELECTROMECHANICAL DESIGN, MODELING AND IMPLEMENTATION OF

    E-Print Network [OSTI]

    Kochersberger, Kevin

    AERODYNAMIC AND ELECTROMECHANICAL DESIGN, MODELING AND IMPLEMENTATION OF PIEZOCOMPOSITE AIRFOILS, Macro-Fiber Composite, Unimorph, Bimorph Onur Bilgen, 2010 #12;AERODYNAMIC AND ELECTROMECHANICAL of the aerodynamic and electromechanical systems that are necessary for a practical implementation

  20. Sandia Energy - Rotor Aerodynamic Design

    Broader source: All U.S. Department of Energy (DOE) Office Webpages (Extended Search)

    AFDC Printable Version Share this resource Send a link to EERE: Alternative Fuels Data Center Home Page to someone by E-mail Share EERE: Alternative Fuels Data Center Home Page on Facebook Tweet about EERE: Alternative Fuels Data Center Home Page on Twitter Bookmark EERE: Alternative Fuels Data Center Homesum_a_epg0_fpd_mmcf_m.xls" ,"Available from WebQuantity ofkandz-cm11 Outreach Home RoomPreservation of Fe(II)Geothermal EnergyRenewable Energy IntegrationRisk and SafetyAerodynamic

  1. 16.100 Aerodynamics, Fall 2002

    E-Print Network [OSTI]

    Darmofal, David L.

    This course extends fluid mechanic concepts from Unified Engineering to the aerodynamic performance of wings and bodies in sub/supersonic regimes. 16.100 generally has four components: subsonic potential flows, including ...

  2. Inequality design limits in optimal aerodynamic shapes

    E-Print Network [OSTI]

    Seaman, Charles Knight

    1968-01-01

    INEQUALITY DESIGN LIMITS IN OPTIMAL AERODYNAMIC SHAPES A Thesis By CHARLES KNIGHT SEAMAN Submitted to the Graduate College of the Texas A&M University in partial fulfillment of the requirements for the degree of MASTER OF SCIENCE May 1968... Major Subject: Aerospace Engineering INEQUALITY DESIGN LIMITS IN OPTIMAL AERODYNAMIC SHAPES A Thesis By CHARLES KNIGHT SEAMAN Approved as to style and content by: (Chairman of Committee) (Head of Department) (Member) (Member) May 1968...

  3. Property:EstimatedCostMedianUSD | Open Energy Information

    Open Energy Info (EERE)

    AFDC Printable Version Share this resource Send a link to EERE: Alternative Fuels Data Center Home Page to someone by E-mail Share EERE: Alternative Fuels Data Center Home Page on Facebook Tweet about EERE: Alternative Fuels Data Center Home Page on Twitter Bookmark EERE: Alternative Fuels Data Center Home Page on Google Bookmark EERE: Alternative Fuels Data Center Home Page on QA:QA J-E-1 SECTION JEnvironmental Jump to: navigation, searchEnvironmentalMitigation Jump to:EstimatedCostMedianUSD

  4. Property:EstimatedTimeMedian | Open Energy Information

    Open Energy Info (EERE)

    AFDC Printable Version Share this resource Send a link to EERE: Alternative Fuels Data Center Home Page to someone by E-mail Share EERE: Alternative Fuels Data Center Home Page on Facebook Tweet about EERE: Alternative Fuels Data Center Home Page on Twitter Bookmark EERE: Alternative Fuels Data Center Home Page on Google Bookmark EERE: Alternative Fuels Data Center Home Page on QA:QA J-E-1 SECTION JEnvironmental Jump to: navigation, searchEnvironmentalMitigationEstimatedTimeMedian Jump to:

  5. Six Degree of Freedom Morphing Aircraft Dynamical Model with Aerodynamics

    E-Print Network [OSTI]

    Niksch, Adam

    2010-01-14

    model of a morphing aircraft is needed. This paper develops an aerodynamic model and a dynamic model of a morphing flying wing aircraft. The dynamic model includes realistic aerodynamic forces, consisting of lift, drag, and pitching moment about...

  6. The Aerodynamic Performance Of Platoons: A Final Report

    E-Print Network [OSTI]

    Zabat, Michael; Stabile, Nick; Farascaroli, Stefano; Browand, Frederick

    1995-01-01

    iii) Measurements of aerodynamic forces in a crosswind.The presence of a crosswind is another important platoon

  7. Computerized method and system for designing an aerodynamic focusing lens stack

    DOE Patents [OSTI]

    Gard, Eric (San Francisco, CA); Riot, Vincent (Oakland, CA); Coffee, Keith (Diablo Grande, CA); Woods, Bruce (Livermore, CA); Tobias, Herbert (Kensington, CA); Birch, Jim (Albany, CA); Weisgraber, Todd (Brentwood, CA)

    2011-11-22

    A computerized method and system for designing an aerodynamic focusing lens stack, using input from a designer related to, for example, particle size range to be considered, characteristics of the gas to be flowed through the system, the upstream temperature and pressure at the top of a first focusing lens, the flow rate through the aerodynamic focusing lens stack equivalent at atmosphere pressure; and a Stokes number range. Based on the design parameters, the method and system determines the total number of focusing lenses and their respective orifice diameters required to focus the particle size range to be considered, by first calculating for the orifice diameter of the first focusing lens in the Stokes formula, and then using that value to determine, in iterative fashion, intermediate flow values which are themselves used to determine the orifice diameters of each succeeding focusing lens in the stack design, with the results being output to a designer. In addition, the Reynolds numbers associated with each focusing lens as well as exit nozzle size may also be determined to enhance the stack design.

  8. AIAA 99--1467 LOW ORDER AERODYNAMIC

    E-Print Network [OSTI]

    Peraire, Jaime

    speeds and more flexible blading, aeroelasticity has become a critical consideration in the design of com will operate within stability boundaries, and thus has a large impact on the design process. Appropriate blade ten per blade passage, making it appropriate for con trol applications. The aerodynamic model

  9. AIAA 20031068 Aerodynamic Design of Cascades by

    E-Print Network [OSTI]

    Liu, Feng

    is developed for the aerodynamic design of cascade blades in a two-dimensional, inviscid, and compressible flow cascade blade design cases are tested. The results show that the method is effective and efficient for turbomachinery blade design. The effect of shape functions on the performance of the design method is discussed

  10. Airfoil Optimization Using Practical Aerodynamic Design Requirements

    E-Print Network [OSTI]

    Zingg, David W.

    to climate change, and rising jet fuel prices are negatively impacting profits of commercial carriers, the design objective of improving aircraft fuel efficiency has become increasingly impor- tant. If it can be shown that a novel aerodynamic shape will provide the greatest improvement in aircraft fuel efficiency

  11. Aerodynamic beam generator for large particles

    DOE Patents [OSTI]

    Brockmann, John E. (Albuquerque, NM); Torczynski, John R. (Albuquerque, NM); Dykhuizen, Ronald C. (Albuquerque, NM); Neiser, Richard A. (Albuquerque, NM); Smith, Mark F. (Albuquerque, NM)

    2002-01-01

    A new type of aerodynamic particle beam generator is disclosed. This generator produces a tightly focused beam of large material particles at velocities ranging from a few feet per second to supersonic speeds, depending on the exact configuration and operating conditions. Such generators are of particular interest for use in additive fabrication techniques.

  12. Electromyographic responses to aerodynamic vs. drop handlebars

    E-Print Network [OSTI]

    Layne, Donald Jodel

    1996-01-01

    that there are no metabolic changes associated with the use of aerodynamic handlebars. These findings are contradicted by anecdotal evidence of specific fatigue and pain in regions such as the upper thigh, buttocks and low back. This anecdotal evidence may point out...

  13. Growth of nanostructures with controlled diameter

    DOE Patents [OSTI]

    Pfefferle, Lisa; Haller, Gary; Ciuparu, Dragos

    2009-02-03

    Transition metal-substituted MCM-41 framework structures with a high degree of structural order and a narrow pore diameter distribution were reproducibly synthesized by a hydrothermal method using a surfactant and an anti-foaming agent. The pore size and the mesoporous volume depend linearly on the surfactant chain length. The transition metals, such as cobalt, are incorporated substitutionally and highly dispersed in the silica framework. Single wall carbon nanotubes with a narrow diameter distribution that correlates with the pore diameter of the catalytic framework structure were prepared by a Boudouard reaction. Nanostructures with a specified diameter or cross-sectional area can therefore be predictably prepared by selecting a suitable pore size of the framework structure.

  14. Freight Wing Trailer Aerodynamics Final Technical Report

    SciTech Connect (OSTI)

    Sean Graham

    2007-10-31

    Freight Wing Incorporated utilized the opportunity presented by a DOE category two Inventions and Innovations grant to commercialize and improve upon aerodynamic technology for semi-tuck trailers, capable of decreasing heavy vehicle fuel consumption, related environmental damage, and U.S. consumption of foreign oil. Major project goals included the demonstration of aerodynamic trailer technology in trucking fleet operations, and the development and testing of second generation products. A great deal of past scientific research has demonstrated that streamlining box shaped semi-trailers can significantly reduce a trucks fuel consumption. However, significant design challenges have prevented past concepts from meeting industry needs. Freight Wing utilized a 2003 category one Inventions and Innovations grant to develop practical solutions to trailer aerodynamics. Fairings developed for the front, rear, and bottom of standard semi-trailers together demonstrated a 7% improvement to fuel economy in scientific tests conducted by the Transportation Research Center (TRC). Operational tests with major trucking fleets proved the functionality of the products, which were subsequently brought to market. This category two grant enabled Freight Wing to further develop, test and commercialize its products, resulting in greatly increased understanding and acceptance of aerodynamic trailer technology. Commercialization was stimulated by offering trucking fleets 50% cost sharing on trial implementations of Freight Wing products for testing and evaluation purposes. Over 230 fairings were implemented through the program with 35 trucking fleets including industry leaders such as Wal-Mart, Frito Lay and Whole Foods. The feedback from these testing partnerships was quite positive with product performance exceeding fleet expectations in many cases. Fleet feedback also was also valuable from a product development standpoint and assisted the design of several second generation products intended to further improve efficiency, lower costs, and enhance durability. Resulting products demonstrated a 30% efficiency improvement in full scale wind tunnel tests. The fuel savings of our most promising product, the Belly Fairing increased from 4% to 6% in scientific track and operational tests. The project successfully demonstrated the economic feasibility of trailer aerodynamics and positioned the technology to realize significant public benefits. Scientific testing conducted with partners such as the EPA Smartway program and Transport Canada clearly validated the fuel and emission saving potential of the technology. The Smartway program now recommends trailer aerodynamics as a certified fuel saving technology and is offering incentives such as low interest loans. Trailer aerodynamics can save average trucks over 1,100 gallons of fuel an 13 tons of emissions every 100,000 miles, a distance many trucks travel annually. These fuel savings produce a product return on investment period of one to two years in average fleet operations. The economic feasibility of the products was validated by participating fleets, several of which have since completed large implementations or demonstrated an interest in volume orders. The commercialization potential of the technology was also demonstrated, resulting in a national distribution and manufacturing partnership with a major industry supplier, Carrier Transicold. Consequently, Freight Wing is well positioned to continue marketing trailer aerodynamics to the trucking industry. The participation of leading fleets in this project served to break down the market skepticism that represents a primary barrier to widespread industry utilization. The benefits of widespread utilization of the technology could be quite significant for both the transportation industry and the public. Trailer aerodynamics could potentially save the U.S. trucking fleet over a billion gallons of fuel and 20 million tons of emissions annually.

  15. Precision wire feeder for small diameter wire

    DOE Patents [OSTI]

    Brandon, Eldon D. (Albuquerque, NM); Hooper, Frederick M. (Albuquerque, NM); Reichenbach, Marvin L. (Albuquerque, NM)

    1992-01-01

    A device for feeding small diameter wire having a diameter less than 0.04 mm (16 mil) to a welding station includes a driving wheel for controllably applying a non-deforming driving force to the wire to move the free end of the wire towards the welding station; and a tension device such as a torque motor for constantly applying a reverse force to the wire in opposition to the driving force to keep the wire taut.

  16. Precision wire feeder for small diameter wire

    DOE Patents [OSTI]

    Brandon, E.D.; Hooper, F.M.; Reichenbach, M.L.

    1992-08-11

    A device for feeding small diameter wire having a diameter less than 0.04 mm (16 mil) to a welding station includes a driving wheel for controllably applying a non-deforming driving force to the wire to move the free end of the wire towards the welding station; and a tension device such as a torque motor for constantly applying a reverse force to the wire in opposition to the driving force to keep the wire taut. 1 figure.

  17. The algebra of metric betweenness II: geometry and equational characterization of weakly median graphs

    E-Print Network [OSTI]

    Chepoi, Victor

    . This demonstrates that the median algebras featured by Avann and Sholander half a century ago and, more generally

  18. Local Stability of the Median LMS Filter W.A. Sethares // J.A. Bucklew

    E-Print Network [OSTI]

    Bucklew, James Antonio

    Local Stability of the Median LMS Filter W.A. Sethares // J.A. Bucklew November 17, 2000 1 #12; Abstract Local stability properties of the recently proposed median LMS adaptive filter are investigated. This will help delineate those applications for which the median LMS is an appropriate adaptive al gorithm

  19. Salt-and-Pepper Noise Removal by Median-type Noise Detectors and

    E-Print Network [OSTI]

    Chan, Raymond

    1 Salt-and-Pepper Noise Removal by Median-type Noise Detectors and Detail-preserving Regularization for removing salt-and-pepper impulse noise. In the first phase, an adaptive median filter is used to identify remove salt-and-pepper-noise with noise level as high as 90%. Index Terms Impulse noise, adaptive median

  20. Device for reducing vehicle aerodynamic resistance

    DOE Patents [OSTI]

    Graham, Sean C.

    2006-03-07

    A device for reducing vehicle aerodynamic resistance for vehicles having a generally rectangular flat front face comprising a plurality of load bearing struts of a predetermined size attached to the flat front face adjacent the sides and top thereof, a pair of pliable opposing flat sheets having an outside edge portion attached to the flat front face adjacent the sides thereof and an upper edge with a predetermined curve; the opposing flat sheets being bent and attached to the struts to form effective curved airfoil shapes, and a top pliable flat sheet disposed adjacent the top of the flat front face and having predetermined curved side edges, which, when the top sheet is bent and attached to the struts to form an effective curved airfoil shape, mate with the curved upper edges of the opposing sheets to complete the aerodynamic device.

  1. Device for reducing vehicle aerodynamic resistance

    DOE Patents [OSTI]

    Graham, Sean C.

    2006-08-22

    A device for reducing vehicle aerodynamic resistance for vehicles having a generally rectangular body disposed above rear wheels, comprising a plurality of load bearing struts attached to the bottom of the rectangular body adjacent its sides, a plurality of opposing flat sheets attached to the load bearing struts, and angled flaps attached to the lower edge of the opposing sheets defining an obtuse angle with the opposing flat sheets extending inwardly with respect to the sides of the rectangular body to a predetermined height above the ground, which, stiffen the opposing flat sheets, bend to resist damage when struck by the ground, and guide airflow around the rear wheels of the vehicle to reduce its aerodynamic resistance when moving.

  2. Device for reducing vehicle aerodynamic resistance

    DOE Patents [OSTI]

    Graham, Sean C.

    2005-02-15

    A device for a vehicle with a pair of swinging rear doors, which converts flat sheets of pliable material hinged to the sides of the vehicle adjacent the rear thereof into effective curved airfoils that reduce the aerodynamic resistance of the vehicle, when the doors are closed by hand, utilizing a plurality of stiffeners disposed generally parallel to the doors and affixed to the sheets and a plurality of collapsible tension bearings struts attached to each stiffener and the adjacent door.

  3. Aerodynamics of a rigid curved kite wing

    E-Print Network [OSTI]

    Maneia, Gianmauro; Tordella, Daniela; Iovieno, Michele

    2013-01-01

    A preliminary numerical study on the aerodynamics of a kite wing for high altitude wind power generators is proposed. Tethered kites are a key element of an innovative wind energy technology, which aims to capture energy from the wind at higher altitudes than conventional wind towers. We present the results obtained from three-dimensional finite volume numerical simulations of the steady air flow past a three-dimensional curved rectangular kite wing (aspect ratio equal to 3.2, Reynolds number equal to 3x10^6). Two angles of incidence -- a standard incidence for the flight of a tethered airfoil (6{\\deg}) and an incidence close to the stall (18{\\deg}) -- were considered. The simulations were performed by solving the Reynolds Averaged Navier-Stokes flow model using the industrial STAR-CCM+ code. The overall aerodynamic characteristics of the kite wing were determined and compared to the aerodynamic characteristics of the flat rectangular non twisted wing with an identical aspect ratio and section (Clark Y profil...

  4. Hybrid method for aerodynamic shape optimization in automotive industry

    E-Print Network [OSTI]

    Dumas, Laurent

    Hybrid method for aerodynamic shape optimization in automotive industry Freedeerique Muyl precisely the reduction of their drag coefficient, becomes one of the main topics of the automotive research

  5. Aerodynamic Focusing Of High-Density Aerosols

    SciTech Connect (OSTI)

    Ruiz, D. E.; Fisch, Nathaniel

    2014-02-24

    High-density micron-sized particle aerosols might form the basis for a number of applications in which a material target with a particular shape might be quickly ionized to form a cylindrical or sheet shaped plasma. A simple experimental device was built in order to study the properties of high-density aerosol focusing for 1#22; m silica spheres. Preliminary results recover previous findings on aerodynamic focusing at low densities. At higher densities, it is demonstrated that the focusing properties change in a way which is consistent with a density dependent Stokes number.

  6. The Aerodynamic, Dual- Wavelength Optical Spectrometer

    Broader source: All U.S. Department of Energy (DOE) Office Webpages (Extended Search)

    AFDC Printable Version Share this resource Send a link to EERE: Alternative Fuels Data Center Home Page to someone by E-mail Share EERE: Alternative Fuels Data Center Home Page on Facebook Tweet about EERE: Alternative Fuels Data Center Home Page on Twitter Bookmark EERE: Alternative Fuels Data Center Homesum_a_epg0_fpd_mmcf_m.xls" ,"Available from WebQuantityBonneville Power AdministrationRobust,Field-effectWorking With U.S. CoalMexicoConferencePriceshieldingFocus TheAerodynamic,

  7. Wind Turbine Blade Flow Fields and Prospects for Active Aerodynamic Control: Preprint

    SciTech Connect (OSTI)

    Schreck, S.; Robinson, M.

    2007-08-01

    This paper describes wind turbine flow fields that can cause adverse aerodynamic loading and can impact active aerodynamic control methodologies currently contemplated for wind turbine applications.

  8. Small diameter, deep bore optical inspection system

    DOE Patents [OSTI]

    Lord, David E. (Livermore, CA); Petrini, Richard R. (Livermore, CA); Carter, Gary W. (Livermore, CA)

    1981-01-01

    An improved rod optic system for inspecting small diameter, deep bores. The system consists of a rod optic system utilizing a curved mirror at the end of the rod lens such that the optical path through the system is bent 90.degree. to minimize optical distortion in examining the sides of a curved bore. The system is particularly useful in the examination of small bores for corrosion, and is capable of examining 1/16 inch diameter and up to 4 inch deep drill holes, for example. The positioning of the curved mirror allows simultaneous viewing from shallow and right angle points of observation of the same artifact (such as corrosion) in the bore hole. The improved rod optic system may be used for direct eye sighting, or in combination with a still camera or a low-light television monitor; particularly low-light color television.

  9. ON THE p-MEDIAN POLYTOPE OF A SPECIAL CLASS OF ...

    E-Print Network [OSTI]

    p-median and the uncapacitated facility location polytopes, the odd cycle ... description of the fractional extreme points of the linear relaxation for the p-

  10. Thread gauge for measuring thread pitch diameters

    DOE Patents [OSTI]

    Brewster, A.L.

    1985-11-19

    A thread gauge which attaches to a vernier caliper to measure the thread pitch diameter of both externally threaded and internally threaded parts is disclosed. A pair of anvils are externally threaded with threads having the same pitch as those of the threaded part. Each anvil is mounted on a stem having a ball on which the anvil can rotate to properly mate with the parts to which the anvils are applied. The stems are detachably secured to the caliper blades by attachment collars having keyhole openings for receiving the stems and caliper blades. A set screw is used to secure each collar on its caliper blade. 2 figs.

  11. Variable diameter wind turbine rotor blades

    DOE Patents [OSTI]

    Jamieson, Peter McKeich; Hornzee-Jones, Chris; Moroz, Emilian M.; Blakemore, Ralph W.

    2005-12-06

    A system and method for changing wind turbine rotor diameters to meet changing wind speeds and control system loads is disclosed. The rotor blades on the wind turbine are able to adjust length by extensions nested within or containing the base blade. The blades can have more than one extension in a variety of configurations. A cable winching system, a hydraulic system, a pneumatic system, inflatable or elastic extensions, and a spring-loaded jack knife deployment are some of the methods of adjustment. The extension is also protected from lightning by a grounding system.

  12. Median regression and the missing information principle Ian W. McKeague

    E-Print Network [OSTI]

    McKeague, Ian

    Median regression and the missing information principle Ian W. McKeague Department of Statistics regression analysis has robustness properties which make it an attractive alternative to regression based of the median regression model, leading to a new estimator for the regression parameters. Our approach adapts

  13. An Efficient Probabilistic Population-Based Descent for the Median Genome Problem

    E-Print Network [OSTI]

    Goëffon, Adrien

    An Efficient Probabilistic Population-Based Descent for the Median Genome Problem Adrien Goëffon@labri.fr ABSTRACT We present a novel population-based local search algorithm for the median genome problem of ancestral genome reconstruc- tion compared to existing methods, making it possible to tackle problems where

  14. Methods of reducing vehicle aerodynamic drag

    SciTech Connect (OSTI)

    Sirenko V.; Rohatgi U.

    2012-07-08

    A small scale model (length 1710 mm) of General Motor SUV was built and tested in the wind tunnel for expected wind conditions and road clearance. Two passive devices, rear screen which is plate behind the car and rear fairing where the end of the car is aerodynamically extended, were incorporated in the model and tested in the wind tunnel for different wind conditions. The conclusion is that rear screen could reduce drag up to 6.5% and rear fairing can reduce the drag by 26%. There were additional tests for front edging and rear vortex generators. The results for drag reduction were mixed. It should be noted that there are aesthetic and practical considerations that may allow only partial implementation of these or any drag reduction options.

  15. Computational Aerodynamic Analysis of Offshore Upwind and Downwind Turbines

    DOE Public Access Gateway for Energy & Science Beta (PAGES Beta)

    Zhao, Qiuying; Sheng, Chunhua; Afjeh, Abdollah

    2014-01-01

    Aerodynamic interactions of the model NREL 5?MW offshore horizontal axis wind turbines (HAWT) are investigated using a high-fidelity computational fluid dynamics (CFD) analysis. Four wind turbine configurations are considered; three-bladed upwind and downwind and two-bladed upwind and downwind configurations, which operate at two different rotor speeds of 12.1 and 16?RPM. In the present study, both steady and unsteady aerodynamic loads, such as the rotor torque, blade hub bending moment, and base the tower bending moment of the tower, are evaluated in detail to provide overall assessment of different wind turbine configurations. Aerodynamic interactions between the rotor and tower are analyzed,moreincluding the rotor wake development downstream. The computational analysis provides insight into aerodynamic performance of the upwind and downwind, two- and three-bladed horizontal axis wind turbines.less

  16. Error estimation and adaptive mesh refinement for aerodynamic flows

    E-Print Network [OSTI]

    Hartmann, Ralf

    Error estimation and adaptive mesh refinement for aerodynamic flows Ralf Hartmann1 and Paul Houston, 38108 Braunschweig, Germany Ralf.Hartmann@dlr.de 2 School of Mathematical Sciences University

  17. MULTITARGET ERROR ESTIMATION AND ADAPTIVITY IN AERODYNAMIC FLOW SIMULATIONS

    E-Print Network [OSTI]

    Hartmann, Ralf

    MULTI­TARGET ERROR ESTIMATION AND ADAPTIVITY IN AERODYNAMIC FLOW SIMULATIONS RALF HARTMANN of Scientific Computing, TU Braunschweig, Germany (Ralf.Hartmann@dlr.de). 1 #12; 2 R. HARTMANN

  18. Error estimation and adaptive mesh refinement for aerodynamic flows

    E-Print Network [OSTI]

    Hartmann, Ralf

    Error estimation and adaptive mesh refinement for aerodynamic flows Ralf Hartmann, Joachim Held), Lilien- thalplatz 7, 38108 Braunschweig, Germany, e-mail: Ralf.Hartmann@dlr.de 1 #12;2 Ralf Hartmann

  19. MULTITARGET ERROR ESTIMATION AND ADAPTIVITY IN AERODYNAMIC FLOW SIMULATIONS

    E-Print Network [OSTI]

    Hartmann, Ralf

    MULTITARGET ERROR ESTIMATION AND ADAPTIVITY IN AERODYNAMIC FLOW SIMULATIONS RALF HARTMANN Abstract, Germany (Ralf.Hartmann@dlr.de). 1 #12;2 R. HARTMANN quantity under consideration. However, in many

  20. Aerodynamic optimization of a solar powered race vehicle

    E-Print Network [OSTI]

    Augenbergs, Peteris K

    2006-01-01

    Aerodynamic optimization was performed on Tesseract, the MIT Solar Electric Vehicle Team's 2003-2005 solar car using Wind Tunnel 8 at Jacobs/Sverdrup Drivability Test Facility in Allen Park, MI. These tests include angle ...

  1. Particle Size Classification of Glass Particles Using Aerodynamic Jet Vectoring

    E-Print Network [OSTI]

    Smith, Barton L.

    Particle Size Classification of Glass Particles Using Aerodynamic Jet Vectoring Zachary E. Humes blowing and suction control flowsflows that are a fraction of the jet flow rateto sharply change

  2. Aerodynamic performance measurements in a counter-rotating aspirated compressor

    E-Print Network [OSTI]

    Onne, Jean-Franois

    2005-01-01

    This thesis is an experimental investigation of the aerodynamic performances of a counter-rotating aspirated compressor. This compressor is implemented in a blow-down facility, which gives rigorous simulation of the ...

  3. Full-scale wind turbine rotor aerodynamics research

    SciTech Connect (OSTI)

    Simms, D A; Butterfield, C P

    1994-11-01

    The United States Department of Energy and the National Renewable Energy Laboratory (NREL) are conducting research to improve wind turbine technology at the NREL National Wind Technology Center (NWTC). One program, the Combined Experiment, has focused on making measurements needed to understand aerodynamic and structural responses of horizontal-axis wind turbines (HAWT). A new phase of this program, the Unsteady Aerodynamics Experiment, will focus on quantifying unsteady aerodynamic phenomena prevalent in stall-controlled HAWTs. Optimally twisted blades and innovative instrumentation and data acquisition systems will be used in these tests. Data can now be acquired and viewed interactively during turbine operations. This paper describes the NREL Unsteady Aerodynamics Experiment and highlights planned future research activities.

  4. Cost-effectiveness of freeway median high occupancy vehicle (HOV) facility conversion to rail guideway transit

    E-Print Network [OSTI]

    Best, Matthew Evans

    1996-01-01

    Many freeways in the United States contain median high occupancy vehicle (HOV) facilities. These facilities have been envisioned by some as reserved space for future rail guideway transit. This thesis examines the cost-effectiveness of converting a...

  5. Development of guidelines for the aesthetic surface treatment of safety-shaped median barriers

    E-Print Network [OSTI]

    Ness, Jacob Raymond

    2004-11-15

    treatment of safety-shaped median barriers. Numerical simulation was utilized to develop these guidelines. This was done by first validating the vehicle model that was used in this research, which was the National Crash Analysis Center (NCAC) 2000P...

  6. Fact #597: November 16, 2009 Median Age of Cars and Trucks Rising in 2008

    Broader source: Energy.gov [DOE]

    The median age of cars and trucks in the U.S. continued to grow in 2008. Due to the economic climate and high gasoline prices that summer, consumers held onto their vehicles longer and delayed new...

  7. DOE Project on Heavy Vehicle Aerodynamic Drag

    SciTech Connect (OSTI)

    McCallen, R; Salari, K; Ortega, J; Castellucci, P; Pointer, D; Browand, F; Ross, J; Storms, B

    2007-01-04

    Class 8 tractor-trailers consume 11-12% of the total US petroleum use. At highway speeds, 65% of the energy expenditure for a Class 8 truck is in overcoming aerodynamic drag. The project objective is to improve fuel economy of Class 8 tractor-trailers by providing guidance on methods of reducing drag by at least 25%. A 25% reduction in drag would present a 12% improvement in fuel economy at highway speeds, equivalent to about 130 midsize tanker ships per year. Specific goals include: (1) Provide guidance to industry in the reduction of aerodynamic drag of heavy truck vehicles; (2) Develop innovative drag reducing concepts that are operationally and economically sound; and (3) Establish a database of experimental, computational, and conceptual design information, and demonstrate the potential of new drag-reduction devices. The studies described herein provide a demonstration of the applicability of the experience developed in the analysis of the standard configuration of the Generic Conventional Model. The modeling practices and procedures developed in prior efforts have been applied directly to the assessment of new configurations including a variety of geometric modifications and add-on devices. Application to the low-drag 'GTS' configuration of the GCM has confirmed that the error in predicted drag coefficients increases as the relative contribution of the base drag resulting from the vehicle wake to the total drag increases and it is recommended that more advanced turbulence modeling strategies be applied under those circumstances. Application to a commercially-developed boat tail device has confirmed that this restriction does not apply to geometries where the relative contribution of the base drag to the total drag is reduced by modifying the geometry in that region. Application to a modified GCM geometry with an open grille and radiator has confirmed that the underbody flow, while important for underhood cooling, has little impact on the drag coefficient of the vehicle. Furthermore, the evaluation of the impact of small changes in radiator or grille dimensions has revealed that the total drag is not particularly sensitive to those changes. This observation leads to two significant conclusions. First, a small increase in radiator size to accommodate heat rejection needs related to new emissions restrictions may be tolerated without significant increases in drag losses. Second, efforts to reduce drag on the tractor requires that the design of the entire tractor be treated in an integrated fashion. Simply reducing the size of the grille will not provide the desired result, but the additional contouring of the vehicle as a whole which may be enabled by the smaller radiator could have a more significant effect.

  8. Product design and development of an aerodynamic hydration system for bicycling and triathlon

    E-Print Network [OSTI]

    Cote, Mark (Mark Brian)

    2007-01-01

    Proper hydration and aerodynamic performance are both essential needs of a competitive cyclist or triathlete. Several aerodynamic systems have been developed for use on bicycles but few have been designed to be truly ...

  9. Film Cooling, Heat Transfer and Aerodynamic Measurements in a Three Stage Research Gas Turbine

    E-Print Network [OSTI]

    Suryanarayanan, Arun

    2010-07-14

    turbine rotational speeds namely, 2400rpm, 2550rpm and 3000rpm. Interstage aerodynamic measurements with miniature five hole probes are also acquired at these speeds. The aerodynamic data characterizes the flow along the first stage rotor exit, second...

  10. Variation in the aerodynamic drag coefficient due to changes in the shape of an automobile

    E-Print Network [OSTI]

    Williams, John Gilbert

    1968-01-01

    . in Gage Bridge Calibration Results 22 Total Strain Gage Bridge Calibration Results 23 13 14 Exterior of' Com'bination Box. Combination Box, Strain Indicator, and Connecting Cables 25 26 15 16 17 Aerodynamic Drag ? Top and. Windows Up... Aerodynamic Drag ? Top and Windows Down Aerodynamic Drag ? Top Down, Windows Up Aerodynamic Drag - Top Up, Windows Down 31 19 Bas"'c Circuit - Combination of Wheat. tone Bridge Outputs 'v Figure Page 20 Equivalent Circui. t - Combination of Vneatstone...

  11. European Conference on Objectoriented Programming (ECOOP) h5index: 28 h5median: 45

    E-Print Network [OSTI]

    Xie, Tao

    European Conference on Objectoriented Programming (ECOOP) h5index: 28 h5median: 45 #17 Software Saftoiu, S Krishnamurthi Proceedings of the 24th European conference on Objectoriented programming ... 109 Vafeiadis Proceedings of the 24th European conference on Objectoriented programming ... 92 2010 JCo

  12. Effects of muscle fiber type and size on EMG median frequency and conduction velocity

    E-Print Network [OSTI]

    De Luca, Carlo J.

    an in vitro method for comparing surface-detected electromyographic median fre- quency (MF) and conduction-sectional area (CSA). Electromyographic sig- nals were recorded during electrically elicited tetanic contrac a muscular contraction are related to muscle fiber type com- position and muscle fiber CSA. electromyographic

  13. Courses for Breadth Requirement of Aerospace Engineering M.S. Degree Aerodynamics,

    E-Print Network [OSTI]

    Gao, Grace Xingxin

    Mechanics, Combustion and Propulsion (AFMCP) AE 410/CSE 461: Computational Aerodynamics AE 412/ME 411 515: Wing Theory AE 538/ ME 501: Combustion Fundamentals AE 598 AAA: Advanced Applied Aerodynamics AE 598 CAA: Aeroacoustics AE 598 CFD: Advanced Computational Aerodynamics AE 598 GSE: Diagnostics

  14. Effect of Dynamic Stall on the Aerodynamics of Vertical-Axis Wind Turbines

    E-Print Network [OSTI]

    McCalley, James D.

    Effect of Dynamic Stall on the Aerodynamics of Vertical-Axis Wind Turbines Frank Scheurich of the aerodynamic performance of vertical-axis wind turbines pose a significant challenge for computational fluid of the aerodynamics of a vertical- axis wind turbine that consists of three curved rotor blades that are twisted

  15. INTRODUCTION 1.1 Aerodynamics of Rotors in Forward Flight

    E-Print Network [OSTI]

    design. In order to capture the above physical phenomena, the influence of the inflow, blade dynamics1 CHAPTER I INTRODUCTION 1.1 Aerodynamics of Rotors in Forward Flight The prediction of rotor blade. Shock induced separation and shock motion along the chord of the blade may occur. Because the inboard

  16. Aerodynamic Optimization Under a Range of Operating Conditions

    E-Print Network [OSTI]

    Zingg, David W.

    Aerodynamic Optimization Under a Range of Operating Conditions David W. Zingg and Samy Elias. This can be achieved through multipoint optimization. The desired performance objective and operating conditions must be speci ed, and the resulting optimization problem must be solved in such a manner

  17. OUTLINE FOR Chapter 5 AERODYNAMICS (W4-2-1)

    E-Print Network [OSTI]

    Leu, Tzong-Shyng "Jeremy"

    Vortex Filament Vortex line Vortex filament: a infinitesimal vortex tube. Vortex tube Reference: "Low Vortex in 3D Airfoil / Lifting Line theory 4 #12;2013/6/3 3 INDUCED VELOCITY, EFFECTIVE ANGLE OF ATTACK4_2_4) OUTLINE FOR Chapter 5 AERODYNAMICS (W4-3-1) #12;2013/6/3 5 Helmholtz Vortex Theorem

  18. Aerodynamic Drag Reduction Apparatus For Wheeled Vehicles In Ground Effect

    DOE Patents [OSTI]

    Ortega, Jason M. (Pacifica, CA); Salari, Kambiz (Livermore, CA)

    2005-12-13

    An apparatus for reducing the aerodynamic drag of a wheeled vehicle in a flowstream, the vehicle having a vehicle body and a wheel assembly supporting the vehicle body. The apparatus includes a baffle assembly adapted to be positioned upstream of the wheel assembly for deflecting airflow away from the wheel assembly so as to reduce the incident pressure on the wheel assembly.

  19. Journal of Wind Engineering and Industrial Aerodynamics 96 (2008) 503523

    E-Print Network [OSTI]

    Manuel, Lance

    2008-01-01

    Journal of Wind Engineering and Industrial Aerodynamics 96 (2008) 503523 On the propagation of uncertainty in inflow turbulence to wind turbine loads Korn Saranyasoontorn, Lance Manuel Department of Civil or design of wind turbines in normal operating states, it is common to use well-established standard

  20. Journal of Wind Engineering and Industrial Aerodynamics 92 (2004) 789804

    E-Print Network [OSTI]

    Manuel, Lance

    2004-01-01

    Journal of Wind Engineering and Industrial Aerodynamics 92 (2004) 789804 Efficient models for wind of wind turbines against extreme loads is the focus of this study. A procedure to establish nominal loads-axis wind turbine. Only operating loads--here, flapwise (out-of-plane) bending moments--at a blade root

  1. Plasma Aerodynamic Control Effectors for Improved Wind Turbine Performance

    SciTech Connect (OSTI)

    Mehul P. Patel; Srikanth Vasudevan; Robert C. Nelson; Thomas C. Corke

    2008-08-01

    Orbital Research Inc is developing an innovative Plasma Aerodynamic Control Effectors (PACE) technology for improved performance of wind turbines. The PACE system is aimed towards the design of "smart" rotor blades to enhance energy capture and reduce aerodynamic loading and noise using flow-control. The PACE system will provide ability to change aerodynamic loads and pitch distribution across the wind turbine blade without any moving surfaces. Additional benefits of the PACE system include reduced blade structure weight and complexity that should translate into a substantially reduced initial cost. During the Phase I program, the ORI-UND Team demonstrated (proof-of-concept) performance improvements on select rotor blade designs using PACE concepts. Control of both 2-D and 3-D flows were demonstrated. An analytical study was conducted to estimate control requirements for the PACE system to maintain control during wind gusts. Finally, independent laboratory experiments were conducted to identify promising dielectric materials for the plasma actuator, and to examine environmental effects (water and dust) on the plasma actuator operation. The proposed PACE system will be capable of capturing additional energy, and reducing aerodynamic loading and noise on wind turbines. Supplementary benefits from the PACE system include reduced blade structure weight and complexity that translates into reduced initial capital costs.

  2. Unsteady Aerodynamic Models for Agile Flight at Low Reynolds Numbers

    E-Print Network [OSTI]

    Rowley, Clarence W.

    for Wagner's and Theodorsen's models, making them compatible with modern control-system analysis. A number thanks are to my advisor, Clancy Rowley, who has been both a role model and a source of encouragementUnsteady Aerodynamic Models for Agile Flight at Low Reynolds Numbers Steven L. Brunton

  3. AERODYNAMICS AND DESIGN FOR ULTRA-LOW REYNOLDS NUMBER FLIGHT

    E-Print Network [OSTI]

    Stanford University

    AERODYNAMICS AND DESIGN FOR ULTRA-LOW REYNOLDS NUMBER FLIGHT A DISSERTATION SUBMITTED at Reynolds numbers below 10,000, here termed ultra-low Reynolds numbers. The effects of airfoil geometry at ultra-low Reynolds numbers. To further explore this design space, the flow solver has been coupled

  4. Journal of Wind Engineering and Industrial Aerodynamics 91 (2003) 15111528

    E-Print Network [OSTI]

    Kareem, Ahsan

    2003-01-01

    flutter was made by Bleich [1] utilizing airfoil flutter theory after the Tacoma Narrows Bridge disaster in aerodynamic tailoring of long span bridges: an advanced analysis framework Xinzhong Chen*, Ahsan Kareem Nat Fitzpatrick Hall, Notre Dame, IN 46556-0767, USA Abstract Significant developments in bridge aeroelastic

  5. AERODYNAMICS (II) Time: Tuesday. 14:00 -17:00

    E-Print Network [OSTI]

    Leu, Tzong-Shyng "Jeremy"

    of forces and moments on, and heat transfer to, bodies moving through a fluid at transonic, supersonic and hypersonic flows. - Lift, drag and moments on the airplanes, missiles . - Aerodynamic heating of space ducts. - Jet engine inlets for transonic, supersonic and hypersonic aircraft. - Ramjet engines

  6. Aerodynamic performance measurements of a film-cooled turbine stage

    E-Print Network [OSTI]

    Keogh, Rory (Rory Colm), 1968-

    2001-01-01

    The goal of this research is to measure the aerodynamic performance of a film-cooled turbine stage and to quantify the loss caused by film-cooling. A secondary goal of the research is to provide a detailed breakdown of the ...

  7. CLARKSON UNIVERSITY AERODYNAMIC FLOW CONTROL OF A HIGH LIFT SYSTEM

    E-Print Network [OSTI]

    Bollt, Erik

    CLARKSON UNIVERSITY AERODYNAMIC FLOW CONTROL OF A HIGH LIFT SYSTEM WITH DUAL SYNTHETIC JET ARRAYS Flow Control of a High Lift System with Dual Synthetic Jet Arrays' presented by Robert Bruce Alstrom the performance of the latest generation aircraft by reducing their fuel consumption and improving their high

  8. Body Force Model for the Aerodynamics of Inclined Perforated Surfaces

    E-Print Network [OSTI]

    Liu, Feng

    Body Force Model for the Aerodynamics of Inclined Perforated Surfaces Juntao Xiong, Andrew Johnson of perforated surfaces inclined to a freestream. The goal is to characterize the key parameters affecting perforations. The model simulates the effects of the perforated surfaces by locally applying a body force term

  9. An Evolutionary Geometry Parametrization for Aerodynamic Shape Optimization

    E-Print Network [OSTI]

    Zingg, David W.

    and greenhouse gas emissions, there is an increase in demand for efficient aircraft with possibly novel, unconventional aerodynamic configurations. Based on improvements in computational fluid dynamics (CFD) and high is not an ideal treatment for an automated optimization process, especially when an unconventional configuration

  10. The Science of Hurricanes Typical eye diameter ~20 miles

    E-Print Network [OSTI]

    Miami, University of

    #12;The Science of Hurricanes #12;#12;Typical eye diameter ~20 miles Typical hurricane diameter-View of a Hurricane #12;Day 0, Disturbance Day 1, 35mph Depression Day 2, 46mph Tropical Storm Day 3, 63mph Tropical Storm Day 4, 92mph Hurricane Day 5, 127mph Hurricane Day 6, 150mph Hurricane Day 7, 144mph Hurricane Day

  11. THE SYNTENIC DIAMETER OF THE SPACE OF NCHROMOSOME

    E-Print Network [OSTI]

    Kleinberg, Jon

    THE SYNTENIC DIAMETER OF THE SPACE OF N­CHROMOSOME GENOMES Jon Kleinberg David Liben similarity among genomes of di#erent species. For each of these measures, a natural but often di#cult problem is to determine the diameter of the space it defines: What is the maximum distance between any pair of genomes

  12. EFFICIENT SERIAL AND PARALLEL ALGORITHMS FOR MEDIAN FILTERING + Sanjay Ranka* and Sartaj Sahni

    E-Print Network [OSTI]

    Sahni, Sartaj K.

    on an N?N image matrix I [1..N, 1..N ] using a W?W window where W = 2w + 1 is an odd number. The result, w, N) and nbhd (b, j, w, N)} where nbhd (p, q, r, s) = ¡ ¢ £ false otherwise true (p - q) mod s r or (q - p) mod s r A straightforward serial computation of MEDIAN2D takes O (N2 W2 ) time

  13. Pressure drop with surface boiling in small-diameter tubes

    E-Print Network [OSTI]

    Dr?mer, Thomas

    1964-01-01

    Pressure drop for water flowing in small-diameter tubes under isothermal, nonboiling, and surface-boiling conditions was investigated. Experimental results for local pressure gradient and heattransfer coefficients are ...

  14. Eddy sensors for small diameter stainless steel tubes.

    SciTech Connect (OSTI)

    Skinner, Jack L.; Morales, Alfredo Martin; Grant, J. Brian; Korellis, Henry James; LaFord, Marianne Elizabeth; Van Blarigan, Benjamin; Andersen, Lisa E.

    2011-08-01

    The goal of this project was to develop non-destructive, minimally disruptive eddy sensors to inspect small diameter stainless steel metal tubes. Modifications to Sandia's Emphasis/EIGER code allowed for the modeling of eddy current bobbin sensors near or around 1/8-inch outer diameter stainless steel tubing. Modeling results indicated that an eddy sensor based on a single axial coil could effectively detect changes in the inner diameter of a stainless steel tubing. Based on the modeling results, sensor coils capable of detecting small changes in the inner diameter of a stainless steel tube were designed, built and tested. The observed sensor response agreed with the results of the modeling and with eddy sensor theory. A separate limited distribution SAND report is being issued demonstrating the application of this sensor.

  15. Diameter dependence of thermoelectric power of semiconducting carbon nanotubes

    E-Print Network [OSTI]

    Hung, Nguyen T.

    We calculate the thermoelectric power (or thermopower) of many semiconducting single wall carbon nanotubes (s-SWNTs) within a diameter range 0.51.5 nm by using the Boltzmann transport formalism combined with an extended ...

  16. Diameter-bandwidth product limitation of isolated-object cloaking

    E-Print Network [OSTI]

    Joannopoulos, John D.

    We show that cloaking of isolated objects using transformation-based cloaks is subject to a diameter-bandwidth product limitation: as the size of the object increases, the bandwidth of good (small-cross-section) cloaking ...

  17. Predicting aerodynamic characteristic of typical wind turbine airfoils using CFD

    SciTech Connect (OSTI)

    Wolfe, W.P. [Sandia National Labs., Albuquerque, NM (United States); Ochs, S.S. [Iowa State Univ., Ames, IA (United States). Aerospace Engineering Dept.

    1997-09-01

    An investigation was conducted into the capabilities and accuracy of a representative computational fluid dynamics code to predict the flow field and aerodynamic characteristics of typical wind-turbine airfoils. Comparisons of the computed pressure and aerodynamic coefficients were made with wind tunnel data. This work highlights two areas in CFD that require further investigation and development in order to enable accurate numerical simulations of flow about current generation wind-turbine airfoils: transition prediction and turbulence modeling. The results show that the laminar-to turbulent transition point must be modeled correctly to get accurate simulations for attached flow. Calculations also show that the standard turbulence model used in most commercial CFD codes, the k-e model, is not appropriate at angles of attack with flow separation. 14 refs., 28 figs., 4 tabs.

  18. Inclusion of nonlinear aerodynamics in the FLAP code

    SciTech Connect (OSTI)

    Weber, T. (Solar Energy Research Inst., Golden, CO (USA)) [Solar Energy Research Inst., Golden, CO (USA)

    1989-11-01

    Horizontal axis wind turbines usually operate with significant portions of the blade in deep stall. This contradicts the assumption in the FLAP code that a linear relation exists between the angle of attack and the lift coefficient. The objective of this paper is to determine the importance of nonlinear aerodynamics in the prediction of loads. The FLAP code has been modified to include the nonlinear relationships between the lift and drag coefficients with the angle of attack. The modification affects the calculation of the induced velocities and the aerodynamic loads. This requires an iterative procedure to determine the induced velocities instead of a closed form solution. A more advanced tower interference model has also been added that accounts for both upwind and downwind tower effects. 7 refs., 14 figs.

  19. Aerodynamic Lightweight Cab Structure Components | Department of Energy

    Office of Energy Efficiency and Renewable Energy (EERE) Indexed Site

    AFDC Printable Version Share this resource Send a link to EERE: Alternative Fuels Data Center Home Page to someone by E-mail Share EERE: Alternative Fuels Data Center Home Page on Facebook Tweet about EERE: Alternative Fuels Data Center Home Page on Twitter Bookmark EERE: Alternative Fuels Data Center Home Page on Google Bookmark EERE: Alternative Fuels Data Center Home Page on Delicious Rank EERE:FinancingPetroleum Based Fuels Research at NREL AdvancedEnergyAdvocate - IssueAerodynamic

  20. DOEs Effort to Reduce Truck Aerodynamic Drag through Joint...

    Office of Energy Efficiency and Renewable Energy (EERE) Indexed Site

    Washington D.C. vss14salari.pdf More Documents & Publications DOEs Effort to Reduce Truck Aerodynamic Drag through Joint Experiments and Computations Vehicle Technologies...

  1. DOEs Effort to Reduce Truck Aerodynamic Drag through Joint...

    Office of Energy Efficiency and Renewable Energy (EERE) Indexed Site

    Meeting vss006salari2012o.pdf More Documents & Publications DOEs Effort to Reduce Truck Aerodynamic Drag through Joint Experiments and Computations Vehicle Technologies...

  2. DOEs Effort to Reduce Truck Aerodynamic Drag through Joint...

    Energy Savers [EERE]

    Truck Aerodynamic Drag through Joint Experiments and Computations 2011 DOE Hydrogen and Fuel Cells Program, and Vehicle Technologies Program Annual Merit Review and Peer...

  3. Additional nuclear criticality safety calculations for small-diameter containers

    SciTech Connect (OSTI)

    Hone, M.J.

    1996-01-01

    This report documents additional criticality safety analysis calculations for small diameter containers, which were originally documented in Reference 1. The results in Reference 1 indicated that some of the small diameter containers did not meet the criteria established for criticality safety at the Portsmouth facility (K{sub eff} +2{sigma}<.95) when modeled under various contingency assumptions of reflection and moderation. The calculations performed in this report reexamine those cases which did not meet the criticality safety criteria. In some cases, unnecessary conservatism is removed, and in other cases mass or assay limits are established for use with the respective containers.

  4. ORIGINAL PAPER Hydraulic properties and embolism in small-diameter

    E-Print Network [OSTI]

    Paris-Sud XI, Universit de

    ORIGINAL PAPER Hydraulic properties and embolism in small-diameter roots of five temperate broad & Context It has been estimated that about half of a plant's total hydraulic resistance is located belowground, but it is not well known how temperate tree species differ in root hydraulic properties and how

  5. Offshore Series Wind Turbine Variable Hub heights & rotor diameters

    E-Print Network [OSTI]

    Firestone, Jeremy

    3.6MW Offshore Series Wind Turbine GE Energy #12;Feature Variable Hub heights & rotor diameters-savings feature, considering the rigors of offshore power generation. The 3.6 MW offshore wind turbine also, for both on and offshore use. Special features include... As the world's first commercially available wind

  6. Absolute Calibration of a Large-diameter Light Source

    E-Print Network [OSTI]

    Brack, J T; Dorofeev, A; Gookin, B; Harton, J L; Petrov, Y; Rovero, A C

    2013-01-01

    A method of absolute calibration for large aperture optical systems is presented, using the example of the Pierre Auger Observatory fluorescence detectors. A 2.5 m diameter light source illuminated by an ultra--violet light emitting diode is calibrated with an overall uncertainty of 2.1 % at a wavelength of 365 nm.

  7. Offshore Series Wind Turbine Variable Hub heights & rotor diameters

    E-Print Network [OSTI]

    Firestone, Jeremy

    3.6MW Offshore Series Wind Turbine GE Energy #12;Feature Variable Hub heights & rotor diameters and providing longer turbine life GE's unique electronics provide transmission efficiencies and enable harmonious function within the local grid Allows wind turbines to stay on line generating power, even during

  8. Nanopatterning Fabrication of a 60-nm-Diameter Perfectly Round

    E-Print Network [OSTI]

    660%. This new technology can be scaled to much larger areas (including roll-to-roll web processing-diameter, perfectly round metal dots over a large area on a polyethylene terephthalate (PET) substrate with high (HSQ) layer on top of PET, nanoimprint litho- graphy, and self-perfection by liquefaction (SPEL

  9. Nuclear criticality safety calculational analysis for small-diameter containers

    SciTech Connect (OSTI)

    LeTellier, M.S.; Smallwood, D.J.; Henkel, J.A. [and others

    1995-11-01

    This report documents calculations performed to establish a technical basis for the nuclear criticality safety of favorable geometry containers, sometimes referred to as 5-inch containers, in use at the Portsmouth Gaseous Diffusion Plant. A list of containers currently used in the plant is shown in Table 1.0-1. These containers are currently used throughout the plant with no mass limits. The use of containers with geometries or material types other than those addressed in this evaluation must be bounded by this analysis or have an additional analysis performed. The following five basic container geometries were modeled and bound all container geometries in Table 1.0-1: (1) 4.32-inch-diameter by 50-inch-high polyethylene bottle; (2) 5.0-inch-diameter by 24-inch-high polyethylene bottle; (3) 5.25-inch-diameter by 24-inch-high steel can ({open_quotes}F-can{close_quotes}); (4) 5.25-inch-diameter by 15-inch-high steel can ({open_quotes}Z-can{close_quotes}); and (5) 5.0-inch-diameter by 9-inch-high polybottle ({open_quotes}CO-4{close_quotes}). Each container type is evaluated using five basic reflection and interaction models that include single containers and multiple containers in normal and in credible abnormal conditions. The uranium materials evaluated are UO{sub 2}F{sub 2}+H{sub 2}O and UF{sub 4}+oil materials at 100% and 10% enrichments and U{sub 3}O{sub 8}, and H{sub 2}O at 100% enrichment. The design basis safe criticality limit for the Portsmouth facility is k{sub eff} + 2{sigma} < 0.95. The KENO study results may be used as the basis for evaluating general use of these containers in the plant.

  10. Advances in Modeling of Aerodynamic Forces on Bridge Xinzhong Chen1

    E-Print Network [OSTI]

    Kareem, Ahsan

    Advances in Modeling of Aerodynamic Forces on Bridge Decks Xinzhong Chen1 and Ahsan Kareem2 be pushing the envelope of the current linear aerodynamics which has successfully served thus far state-of-the-art in this field, may serve as a building block for developing new analysis tools

  11. Aerodynamic Shape Optimization of Airfoils in Ultra-Low Reynolds Number Flow using

    E-Print Network [OSTI]

    Stanford University

    Aerodynamic Shape Optimization of Airfoils in Ultra-Low Reynolds Number Flow using Simultaneous;Aerodynamic Shape Optimization of Airfoils in Ultra-Low Reynolds Number Flow using Simultaneous Pseudo Abstract. The paper presents numerical results of optimized airfoils at ultra-low Reynolds numbers

  12. Fluidic Control of a Turret Wake: Aerodynamic and Aero-Optical Effects

    E-Print Network [OSTI]

    Gordeyev, Stanislav

    Fluidic Control of a Turret Wake: Aerodynamic and Aero-Optical Effects Bojan Vukasinovic and Ari, Missouri 63166 DOI: 10.2514/1.J050085 Effects of direct small-scale actuation on aerodynamic and aero of separation. Effects of actuation on aero-optical distortions are assessed from the flow dynamics, using

  13. WIND-TUNNEL STUDY ON AERODYNAMIC PERFORMANCE OF SMALL VERTICAL-AXIS WIND TURBINES

    E-Print Network [OSTI]

    Leu, Tzong-Shyng "Jeremy"

    1 WIND-TUNNEL STUDY ON AERODYNAMIC PERFORMANCE OF SMALL VERTICAL-AXIS WIND TURBINES J. J. Miau*1 were carried out to study the aerodynamic performance of three vertical axis wind turbines (VAWTs vertical-axis wind turbines (VAWT) have attracted a great deal of attention, because of their potential

  14. Diameter dependent thermoelectric properties of individual SnTe nanowires

    DOE Public Access Gateway for Energy & Science Beta (PAGES Beta)

    Xu, E. Z.; Li, Z.; Martinez, J. A.; Sinitsyn, N.; Htoon, H.; Li, Nan; Swartzentruber, B.; Hollingsworth, J. A.; Wang, Jian; Zhang, S. X.

    2015-01-15

    The lead-free compound tin telluride (SnTe) has recently been suggested to be a potentially promising thermoelectric material because of its similar electronic band structure as the well-known lead telluride. Here we report on the first thermoelectric study of individual single crystalline SnTe nanowires (NWs) with different diameters ranging from ~200 to ~1000 nm. Measurements of thermopower S, electrical conductivity ?, and thermal conductivity ? were carried out on the same nanowires over a temperature range of 25 - 300 K. While ? does not show a strong diameter dependence, the thermopower increases by a factor of 2 when the nanowiremorediameter is decreased from 1000 nm to 200 nm. The thermal conductivities of the measured NWs are only about half of that of the bulk SnTe, which may arise from the enhanced phonon-grain boundary and phonon-defect scatterings. Temperature dependent figure-of-merit ZT was determined and the maximum value at room temperature is ~3 times higher than what was obtained in bulk samples of comparable carrier density.less

  15. Time-delay Cosmography: Increased Leverage with Angular Diameter Distances

    E-Print Network [OSTI]

    Jee, Inh; Suyu, Sherry H; Huterer, Dragan

    2015-01-01

    Strong lensing time-delay systems constrain cosmological parameters via the so-called time-delay distance and the angular diameter distance to the lens. In previous studies, only the former information was used. In this paper, we show that the cosmological constraints improve significantly when the latter information is also included. Specifically, the angular diameter distance plays a crucial role in breaking the degeneracy between the curvature of the Universe and the time-varying equation of state of dark energy. Using a mock sample of 55 bright quadruple lens systems based on expectations for ongoing/future imaging surveys, we find that adding the angular diameter distance information to the time-delay distance information and the cosmic microwave background data of Planck improves the constraint on the constant equation of state by 30%, on the time variation in the equation of state by a factor of two, and on the Hubble constant in the flat $\\Lambda$CDM model by a factor of two. Therefore, previous forec...

  16. Aeroacoustics and aerodynamic performance of a rotor with flatback airfoils.

    SciTech Connect (OSTI)

    Paquette, Joshua A.; Barone, Matthew Franklin; Christiansen, Monica; Simley, Eric

    2010-06-01

    The aerodynamic performance and aeroacoustic noise sources of a rotor employing flatback airfoils have been studied in field test campaign and companion modeling effort. The field test measurements of a sub-scale rotor employing nine meter blades include both performance measurements and acoustic measurements. The acoustic measurements are obtained using a 45 microphone beamforming array, enabling identification of both noise source amplitude and position. Semi-empirical models of flatback airfoil blunt trailing edge noise are developed and calibrated using available aeroacoustic wind tunnel test data. The model results and measurements indicate that flatback airfoil noise is less than drive train noise for the current test turbine. It is also demonstrated that the commonly used Brooks, Pope, and Marcolini model for blunt trailing edge noise may be over-conservative in predicting flatback airfoil noise for wind turbine applications.

  17. Sparse polynomial surrogates for aerodynamic computations with random inputs

    E-Print Network [OSTI]

    Savin, Eric; Peter, Jacques

    2015-01-01

    This paper deals with some of the methodologies used to construct polynomial surrogate models based on generalized polynomial chaos (gPC) expansions for applications to uncertainty quantification (UQ) in aerodynamic computations. A core ingredient in gPC expansions is the choice of a dedicated sampling strategy, so as to define the most significant scenarios to be considered for the construction of such metamodels. A desirable feature of the proposed rules shall be their ability to handle several random inputs simultaneously. Methods to identify the relative "importance" of those variables or uncertain data shall be ideally considered as well. The present work is more particularly dedicated to the development of sampling strategies based on sparsity principles. Sparse multi-dimensional cubature rules based on general one-dimensional Gauss-Jacobi-type quadratures are first addressed. These sets are non nested, but they are well adapted to the probability density functions with compact support for the random in...

  18. Vacuum chamber with a supersonic flow aerodynamic window

    DOE Patents [OSTI]

    Hanson, Clark L. (Livermore, CA)

    1982-01-01

    A supersonic flow aerodynamic window, whereby a steam ejector situated in a primary chamber at vacuum exhausts superheated steam toward an orifice to a region of higher pressure, creating a barrier to the gas in the region of higher pressure which attempts to enter through the orifice. In a mixing chamber outside and in fluid communication with the primary chamber, superheated steam and gas are combined into a mixture which then enters the primary chamber through the orifice. At the point of impact of the ejector/superheated steam and the incoming gas/superheated steam mixture, a barrier is created to the gas attempting to enter the ejector chamber. This barrier, coupled with suitable vacuum pumping means and cooling means, serves to keep the steam ejector and primary chamber at a negative pressure, even though the primary chamber has an orifice to a region of higher pressure.

  19. Vacuum chamber with a supersonic-flow aerodynamic window

    DOE Patents [OSTI]

    Hanson, C.L.

    1980-10-14

    A supersonic flow aerodynamic window is disclosed whereby a steam ejector situated in a primary chamber at vacuum exhausts superheated steam toward an orifice to a region of higher pressure, creating a barrier to the gas in the region of higher pressure which attempts to enter through the orifice. In a mixing chamber outside and in fluid communication with the primary chamber, superheated steam and gas are combined into a mixture which then enters the primary chamber through the orifice. At the point of impact of the ejector/superheated steam and the incoming gas/superheated steam mixture, a barrier is created to the gas attempting to enter the ejector chamber. This barrier, coupled with suitable vacuum pumping means and cooling means, serves to keep the steam ejector and primary chamber at a negative pressure, even though the primary chamber has an orifice to a region of higher pressure.

  20. Aerodynamic testing of a rotating wind turbine blade

    SciTech Connect (OSTI)

    Butterfield, C.P.; Nelsen, E.N.

    1990-01-01

    Aerodynamic, load, flow-visualization, and inflow measurements were taken on a downwind horizontal-axis wind turbine (HAWT). A video camera mounted on the rotor recorded video images of tufts attached to the low-pressure side of the blade. Strain gages, mounted every 10% of the blade's span, provided load and pressure measurements. Pressure taps at 32 chordwise positions recorded pressure distributions. Wind inflow was measured via a vertical-plane array of anemometers located 10 m upwind. The objectives of the test were to address whether airfoil pressure distributions measured on a rotating blade differed from those measured in the wind tunnel, if radial flow near or in the boundary layer of the airfoil affected pressure distributions, if dynamic stall could result in increased dynamic loads, and if the location of the separation boundary measured on the rotating blade agreed with that measured in two-dimensional flow in the wind tunnel. 6 refs., 9 figs., 1 tab.

  1. A comparison of baseline aerodynamic performance of optimally-twisted versus non-twisted HAWT blades

    SciTech Connect (OSTI)

    Simms, D.A.; Robinson, M.C.; Hand, M.M.; Fingersh, L.J.

    1995-01-01

    NREL has completed the initial twisted blade field tests of the ``Unsteady Aerodynamics Experiment.`` This test series continues systematic measurements of unsteady aerodynamic phenomena prevalent in stall-controlled horizontal axis wind turbines (HAWTs). The blade twist distribution optimizes power production at a single angle of attack along the span. Abrupt transitions into and out of stall are created due to rapid changes in inflow. Data from earlier experiments have been analyzed extensively to characterize the steady and unsteady response of untwisted blades. In this report, a characterization and comparison of the baseline aerodynamic performance of the twisted versus non-twisted blade sets will be presented for steady flow conditions.

  2. Allowable pillar to diameter ratio for strategic petroleum reserve caverns.

    SciTech Connect (OSTI)

    Ehgartner, Brian L.; Park, Byoung Yoon

    2011-05-01

    This report compiles 3-D finite element analyses performed to evaluate the stability of Strategic Petroleum Reserve (SPR) caverns over multiple leach cycles. When oil is withdrawn from a cavern in salt using freshwater, the cavern enlarges. As a result, the pillar separating caverns in the SPR fields is reduced over time due to usage of the reserve. The enlarged cavern diameters and smaller pillars reduce underground stability. Advances in geomechanics modeling enable the allowable pillar to diameter ratio (P/D) to be defined. Prior to such modeling capabilities, the allowable P/D was established as 1.78 based on some very limited experience in other cavern fields. While appropriate for 1980, the ratio conservatively limits the allowable number of oil drawdowns and hence limits the overall utility and life of the SPR cavern field. Analyses from all four cavern fields are evaluated along with operating experience gained over the past 30 years to define a new P/D for the reserve. A new ratio of 1.0 is recommended. This ratio is applicable only to existing SPR caverns.

  3. Radiofrequency Ablation of Large Renal Angiomyolipoma: Median-Term Follow-Up

    SciTech Connect (OSTI)

    Gregory, S. M. Anderson, C. J.; Patel, U.

    2013-06-15

    Purpose. To study the feasibility of percutaneous radiofrequency ablation (RFA) of large angiomyolipomas (AMLs) using saline-cooled electrodes. Materials and Methods. Institutional Review Board approval for the study was received. Four patients (all female, age range 33-67 years) with large AMLs (maximal axis 6.1-32.4 cm) not suitable for embolotherapy or surgery consented to a trial of RFA. Procedures were performed under computerized tomographic guidance using 14G saline-infused electrodes. Two ablations (diameter 4-7 cm) were undertaken in each patient. Variables studied were technical success, treatment safety, alteration of tumor consistency, tumor size, effect on renal function, and medium-term freedom from haemorrhage. Results. All four patients underwent successful RFA without any intraprocedural complications. There has been no haemorrhage, or new renal specific symptom, during a minimum 48-month period, and normal renal function has been normal. On follow-up radiological imaging, the tumors have become fattier with involution of the soft-tissue elements (soft tissue-to-total tumor ratio decreased mean [range] of 0.26 [0.14-0.48] to 0.17 [0.04-0.34] U; p = 0.04 [paired Student t test]). Further evidence of treatment effect was the development of a capsule around the ablation zone, but there was no change in overall tumor volume (mean [range] 1,120 [118-2,845] to 1150 [90-3,013] ml; p = 1 [paired Student t test]). Conclusion. RFA of large AMLs is technically feasible using saline-infused electrodes. The soft-tissue elements decreased in volume; the tumors become fattier; and there has been no renal haemorrhage during a 48-month period.

  4. IEEE/ACM International Conference on Automated Software Engineering (ASE) h5-index: 34 h5-median: 50

    E-Print Network [OSTI]

    Xie, Tao

    IEEE/ACM International Conference on Automated Software Engineering (ASE) h5-index: 34 h5-median source code on the web S Thummalapenta, T Xie Proceedings of the twenty-second IEEE/ACM international, Z Hu, H Zhao, M Takeichi, H Mei Proceedings of the twenty-second IEEE/ACM international conference

  5. Unsteady Aerodynamic and Dynamic Analysis of the Meridian UAS in a Rolling-Yawing Motion

    E-Print Network [OSTI]

    Lykins, Ryan

    2014-05-31

    The nonlinear and unsteady aerodynamic effects of operating the Meridian unmanned aerial system (UAS) in crosswinds and at high angular rates is investigated in this work. The Meridian UAS is a large autonomous aircraft, with a V-tail configuration...

  6. Error estimation and anisotropic mesh refinement for 3d laminar aerodynamic flow simulations

    E-Print Network [OSTI]

    Hartmann, Ralf

    Leichta,b , Ralf Hartmann,a,b aInstitute of Aerodynamics and Flow Technology, DLR (German Aerospace Center.Leicht@dlr.de (Tobias Leicht), Ralf.Hartmann@dlr.de (Ralf Hartmann) Preprint submitted to Journal of Computational

  7. Challenges in Simulation of Aerodynamics, Hydrodynamics, and Mooring-Line Dynamics of Floating Offshore Wind Turbines

    SciTech Connect (OSTI)

    Matha, D.; Schlipf, M.; Cordle, A.; Pereira, R.; Jonkman, J.

    2011-10-01

    This paper presents the current major modeling challenges for floating offshore wind turbine design tools and describes aerodynamic and hydrodynamic effects due to rotor and platform motions and usage of non-slender support structures.

  8. Physically-based aerodynamic flight of birds: an interactive approach to behavioral flocking

    E-Print Network [OSTI]

    Ringham, Michael Lynn

    1996-01-01

    This thesis describes a method for simulating the flight of birds in a flock with the use of physically-based aerodynamics. The resulting flocking behavior dramatically improves on results previously obtained in computer graphics and animation...

  9. FY2003 Annual Report: DOE Project on Heavy Vehicle Aerodynamic Drag

    SciTech Connect (OSTI)

    McCallen, R C; Salari, K; Ortega, J; DeChant, L J; Roy, C J; Payne, J J; Hassan, B; Pointer, W D; Browand, F; Hammache, M; Hsu, T; Ross, J; Satran, D; Heineck, J; Walker, S; Yaste, D; Englar, R; Leonard, A; Rubel, M; Chatelain, P

    2003-10-24

    Objective: {sm_bullet} Provide guidance to industry in the reduction of aerodynamic drag of heavy truck vehicles. {sm_bullet} Establish a database of experimental, computational, and conceptual design information, and demonstrate potential of new drag-reduction devices.

  10. Influence of low-speed aerodynamic performance on airport community noise

    E-Print Network [OSTI]

    March, Andrew I. (Andrew Irving)

    2008-01-01

    Properly assessing proposed aviation policies requires a thorough trade study of noise, emissions, fuel consumption, and cost. Aircraft low-speed aerodynamic performance is an important driver of all these impacts, and ...

  11. An acoustic and aerodynamic study of stops in tonal and non-tonal dialects of Korean

    E-Print Network [OSTI]

    Lee, Hyunjung

    2010-03-29

    ABSTRACT This study investigates the acoustic and aerodynamic properties of well&ndashknown three&ndashway distinction of Korean voiceless stops in two dialects, which differ in their tonal systems: non&ndashtonal Seoul Korean (standard Korean...

  12. An aerodynamic surface to deploy and position a stall deterrent spoiler

    E-Print Network [OSTI]

    Brown, Jeffrey Reed

    1974-01-01

    AN AERODYNAMIC SURFACE TO DEPLOY AND POSITION A STALL DETERRENT SPOILER A Thesis JEFFREY REED BROWN Submitted to the Graduate College of Texas A8M University in partial fulfillment of the requirement for the degree of MASTER OF SCIENCE... December 1974 Major Subject: Aerospace Engineering AN AERODYNAMIC SURFACE TO DEPLOY AND POSITION A STALL DETERRENT SPOILER A Thesis by JEFFREY REED BROWN Approved as to style and content by: Chairman of Committee Head o Departm nt Member Member...

  13. Comparison of the Coulter Multisizer and Aerodynamic Particle Sizer for obtaining the aerodynamic particle size of irregularly shaped dust

    E-Print Network [OSTI]

    McClure, Joshua Wayne

    2002-01-01

    properties of the particles. Another method uses the Coulter Multisizer, which measures the volume of each particle that has been collected on a filter. An equivalent diameter for each particle can be found by assuming the particle is spherical, which can...

  14. Diameter Control and Photoluminescence of ZnO Nanorods from Trialkylamines

    DOE Public Access Gateway for Energy & Science Beta (PAGES Beta)

    Andelman, Tamar; Gong, Yinyan; Neumark, Gertrude; O'Brien, Stephen

    2007-01-01

    A novel solution method to control the diameter of ZnO nanorods is reported. Small diameter (2-3 nm) nanorods were synthesized from trihexylamine, and large diameter (5080 nm) nanorods were synthesized by increasing the alkyl chain length to tridodecylamine. The defect (green) emission of the photoluminescence (PL) spectra of the nanorods varies with diameter, and can thus be controlled by the diameter control. The small ZnO nanorods have strong green emission, while the large diameter nanorods exhibit a remarkably suppressed green band. We show that this observation supports surface oxygen vacancies as the defect that gives rise to the green emission.

  15. Small diameter horizontal hole drilling - state of technology

    SciTech Connect (OSTI)

    NONE

    1984-11-01

    The purpose of this study is to determine the existing state of the art for small diameter, horizontal pilot hole drilling. The data were collected by contacting worldwide owners of raise or slant hole drill equipment, manufacturers of drills and bits, and manufacturers of survey tools. The study was limited to existing equipment and completed trials. Most attempts at directional pilot hole drilling, and most survey tools are designed for near vertical, downward drilling. Several types of controllable bits are available which depend upon in-hole motors and bent or wedged assemblies to bias the direction of drilling. Accurate horizontal drilling can be achieved in this way by alternately drilling and surveying at frequent intervals. This procedure is impractical, however, from both a production and a cost standpoint. A few attempts at directional drilling have been made using ordinary drilling tools, a rotary drill string and a tricone bit. Good equipment and a well trained drill crew appeared to be the most significant factor in practical, accurate drilling, whether horizontal or vertical. Because of the cost, no one uses steerable bit drilling except for correction, and then only for short portions of an overall drill program. No satisfactory continuous readout surveying tool, coupled with a remotely controlled bit capable of direction correction, exists. An industry need exists for a high speed, directional drill bit, coupled with a continuously monitored survey tool. 2 tables.

  16. Pulling of 3 mm diameter AlSb rods by micro-pulling down method

    E-Print Network [OSTI]

    Bourret-Courchesne Ph.D., Edith

    2009-01-01

    SUBCONTRACT #6836278 Pulling of 3 mm diameter AlSb rods by1 cm long, and at least 3 mm in diameter. provided by LBNL.l Crucible Power/T Speed (mm/min) Seed Results Crucible

  17. Carbon 39 (2001) 17171722 Electrical resistivity of submicron-diameter carbon-filament

    E-Print Network [OSTI]

    Chung, Deborah D.L.

    2001-01-01

    the filament diameter from 0.05 to 0.16 mm, and also by graphitization of the filaments. The use of nickel filaments will fall. According to Applied nanotubes [3], which typically have diameters in the Sciences Inc

  18. NWTC Aerodynamics Studies Improve Energy Capture and Lower Costs of Wind-Generated Electricity

    SciTech Connect (OSTI)

    2015-08-01

    Researchers at the National Wind Technology Center (NWTC) at the National Renewable Energy Laboratory (NREL) have expanded wind turbine aerodynamic research from blade and rotor aerodynamics to wind plant and atmospheric inflow effects. The energy capture from wind plants is dependent on all of these aerodynamic interactions. Research at the NWTC is crucial to understanding how wind turbines function in large, multiple-row wind plants. These conditions impact the cumulative fatigue damage of turbine structural components that ultimately effect the useful lifetime of wind turbines. This work also is essential for understanding and maximizing turbine and wind plant energy production. Both turbine lifetime and wind plant energy production are key determinants of the cost of wind-generated electricity.

  19. Aerodynamic Drag of Heavy Vehicles (Class 7-8): Simulation and Benchmarking

    SciTech Connect (OSTI)

    Rose McCallen, Dan Flowers, Tim Dunn; Jerry Owens; Fred Browand; Mustapha Hammache; Anthony Leonard; Mark Brady; Kambiz Salari; Walter Rutledge; James Ross; Bruce Storms; J. T. Heineck, David Driver; James Bell; Steve Walker; Gregory Zilliac

    2000-06-19

    This paper describes research and development for reducing the aerodynamic drag of heavy vehicles by demonstrating new approaches for the numerical simulation and analysis of aerodynamic flow. Experimental validation of new computational fluid dynamics methods are also an important part of this approach. Experiments on a model of an integrated tractor-trailer are underway at NASA Ames Research Center and the University of Southern California (USC). Companion computer simulations are being performed by Sandia National Laboratories (SNL), Lawrence Livermore National Laboratory (LLNL), and California Institute of Technology (Caltech) using state-of-the-art techniques.

  20. arXiv:0911.4733v1[cond-mat.mtrl-sci]24Nov2009 Aerodynamical Effects in Snow Crystal Growth

    E-Print Network [OSTI]

    Libbrecht, Kenneth G.

    arXiv:0911.4733v1[cond-mat.mtrl-sci]24Nov2009 Aerodynamical Effects in Snow Crystal Growth K. G review several aspects of aerodynamics that affect the growth, morphology, and symmetry of snow crystals. We derive quantitative estimates for aerodynamical forces that orient falling snow crystals, estimate

  1. Catalyst and its diameter dependent growth kinetics of CVD grown GaN nanowires

    SciTech Connect (OSTI)

    Samanta, Chandan [Department of Physics, Indian Institute of Technology Kanpur (India)] [Department of Physics, Indian Institute of Technology Kanpur (India); Chander, D. Sathish [Department of Physics, Indian Institute of Technology Kanpur (India) [Department of Physics, Indian Institute of Technology Kanpur (India); Department of Mechanical Engineering, Indian Institute of Technology Kanpur (India); Ramkumar, J. [Department of Mechanical Engineering, Indian Institute of Technology Kanpur (India)] [Department of Mechanical Engineering, Indian Institute of Technology Kanpur (India); Dhamodaran, S., E-mail: kdams2003@gmail.com [Department of Physics, Indian Institute of Technology Kanpur (India)

    2012-04-15

    Graphical abstract: GaN nanowires with controlled diameter and aspect ratio has been grown using a simple CVD technique. The growth kinetics of CVD grown nanowires investigated in detail for different catalysts and their diameters. A critical diameter important to distinguish the growth regimes has been discussed in detail. The results are important which demonstrates the growth of diameter and aspect ratio controlled GaN nanowires and also understand their growth kinetics. Highlights: Black-Right-Pointing-Pointer Controlled diameter and aspect ratio of GaN nanowires achieved in simple CVD reactor. Black-Right-Pointing-Pointer Nanowire growth kinetics for different catalyst and its diameters were understood. Black-Right-Pointing-Pointer Adatoms vapor pressure inside reactor plays a crucial role in growth kinetics. Black-Right-Pointing-Pointer Diffusion along nanowire sidewalls dominate for gold and nickel catalysts. Black-Right-Pointing-Pointer Gibbs-Thomson effect dominates for palladium catalyst. -- Abstract: GaN nanowires were grown using chemical vapor deposition with controlled aspect ratio. The catalyst and catalyst-diameter dependent growth kinetics is investigated in detail. We first discuss gold catalyst diameter dependent growth kinetics and subsequently compare with nickel and palladium catalyst. For different diameters of gold catalyst there was hardly any variation in the length of the nanowires but for other catalysts with different diameter a strong length variation of the nanowires was observed. We calculated the critical diameter dependence on adatoms pressure inside the reactor and inside the catalytic particle. This gives an increasing trend in critical diameter as per the order gold, nickel and palladium for the current set of experimental conditions. Based on the critical diameter, with gold and nickel catalyst the nanowire growth was understood to be governed by limited surface diffusion of adatoms and by Gibbs-Thomson effect for the palladium catalyst.

  2. Heat Transfer -1 Consider a composite pipe of inner diameter 10 cm and outer diameter 10.6 cm subjected to an external

    E-Print Network [OSTI]

    Virginia Tech

    Heat Transfer - 1 Consider a composite pipe of inner diameter 10 cm and outer diameter 10.6 cm subjected to an external constant uniform heat flux of 100,000 W/m2 . The composite material of the pipe has/mK in the axial direction. Both ends of the pipe are insulated from any heat loss. The pipe is cooled by water

  3. Global Optimization Methods for the Aerodynamic Shape Design of Transonic Cascades

    E-Print Network [OSTI]

    Neumaier, Arnold

    Global Optimization Methods for the Aerodynamic Shape Design of Transonic Cascades T. Mengistu, Canada Email: mengistu@me.concordia.ca, ghaly@alcor.concordia.ca ABSTRACT Two global optimization shape optimization of transonic cascades; the objective being the redesign of an existing turbomachine

  4. The Natural Aerodynamic Sampling of Trace Explosives from the Human Body

    E-Print Network [OSTI]

    Settles, Gary S.

    The Natural Aerodynamic Sampling of Trace Explosives from the Human Body Gary S. Settles, Huban A. Gowadia, Sean B. Strine, and Timothy E. Johnson Gas Dynamics Lab, Mechanical Engineering Dept., 301D Reber developed for this purpose, their widespread use may be too slow for airport security use and may

  5. Numerical Investigation of Aerodynamic Performance and Loads of a Novel Dual Rotor Wind Turbine

    E-Print Network [OSTI]

    Hu, Hui

    Numerical Investigation of Aerodynamic Performance and Loads of a Novel Dual Rotor Wind Turbine-rotor wind turbine (DRWT) proposed by Rosenberg et al.1 Assuming that the turbine operates in isolation. Comparisons are drawn with the corresponding analyses of a com- parable conventional single-rotor wind turbine

  6. Advanced Flow Diagnostics and Experimental Aerodynamics Laboratory Department of Aerospace Engineering

    E-Print Network [OSTI]

    Hu, Hui

    of complex thermal-flow phenomena: Renewable Energy, wind energy, wind turbine aeromechanics. Bio-flows and micro-scale heat transfer. Icing physics, aircraft icing, power line icing and wind turbine icing. Low-speed aerodynamics, laminar boundary layer separation, transition and flow control. Wind

  7. Fan Aerodynamic Performance Guarantees: Do Your Policies, Procedures and Penalties Provide Adequate Certainty?

    E-Print Network [OSTI]

    Kaufman, S. G.; Martin, V.; Falk, M. A.

    2004-01-01

    With few exceptions, fan vendors do not provide a written guarantee regarding aerodynamic performance. Some fan vendors even go so far as to state in their terms and conditions of sale that fan performance is not guaranteed unless it is specifically...

  8. Supersonic Bi-Directional Flying Wing Configuration with Low Sonic Boom and High Aerodynamic Efficiency

    E-Print Network [OSTI]

    Zha, Gecheng

    that propagates to ground from the shock waves created by a supersonic airplane and its components. PlotkinSupersonic Bi-Directional Flying Wing Configuration with Low Sonic Boom and High Aerodynamic@miami.edu Abstract In this paper, a parametric study is conducted to optimize a business jet using supersonic bi

  9. Five Year Plan Update Staff 631 Helicopter Aerodynamics I X X X X X X

    E-Print Network [OSTI]

    Bernstein, Joseph B.

    788W Smart Fluids and Applications X X X Aerodynamics & Propulsion Sedwick 663 Intro to Plasmas X X X Lee 652 Computational Structural Mechanics X X X X X X Lee 653 Nonlinear Finite Element Analysis X X Wereley 654 Mechanics of Composite Structures X X X Balachandran/Hubbard 655 Structural

  10. Co-Flow Jet Airfoil Trade Study Part I : Energy Consumption and Aerodynamic Efficiency

    E-Print Network [OSTI]

    Zha, Gecheng

    Co-Flow Jet Airfoil Trade Study Part I : Energy Consumption and Aerodynamic Efficiency Alexis airfoils. A trade study is performed for a series of CFJ airfoils based on the NACA 23121 airfoil Static pressure Air density m Mass flow M Mach number Pitching Moment P Pumping power Free stream

  11. Benchmark of aerodynamic cycling helmets using a refined wind tunnel test protocol for helmet drag research

    E-Print Network [OSTI]

    Sidelko, Stephanie

    2007-01-01

    The study of aerodynamics is very important in the world of cycling. Wind tunnel research is conducted on most of the equipment that is used by a rider and is a critical factor in the advancement of the sport. However, to ...

  12. Aerodynamic and Performance Measurements on a SWT-2.3-101 Wind Turbine

    SciTech Connect (OSTI)

    Medina, P.; Singh, M.; Johansen, J.; Jove, A.R.; Machefaux, E.; Fingersh, L. J.; Schreck, S.

    2011-10-01

    This paper provides an overview of a detailed wind turbine field experiment being conducted at NREL under U.S. Department of Energy sponsorship. The purpose of the experiment is to obtain knowledge about the aerodynamics, performance, noise emission and structural characteristics of the Siemens SWT-2.3-101 wind turbine.

  13. CONSTRUCTION AND TESTING OF THE TWO METER DIAMETER TPC THIN SUPERCONDUCTING SOLENOID

    E-Print Network [OSTI]

    Green, M.A.

    2010-01-01

    DIAMETER TPC THIN SUPERCONDUCTING SOLENOID . 'i.A. Green,an Aluminum Stabilized Superconductor", Cryogenics 17, Vol.and Construction of a Superconducting Stabilized Aluminum

  14. Method and apparatus for determining diameter and wall thickness of minute hollow spherical shells

    DOE Patents [OSTI]

    Steinman, D.A.

    1980-05-30

    Method and apparatus for determining diameter and wall thickness of hollow microspheres or shells wherein terminal velocities of shells traveling in fluid-filled conduits of differing diameters are measured. A wall-effect factor is determined as a ratio of the terminal velocities, and shell outside diameter may then be ascertained as a predetermined empirical function of wall-effect factor. For shells of known outside diameter, wall thickness may then be ascertained as a predetermined empirical function of terminal velocity in either conduit.

  15. An approach for the development of an aerodynamic-structural interaction numerical simulation for aeropropulsion systems

    SciTech Connect (OSTI)

    Naziar, J.; Couch, R.; Davis, M.

    1996-01-01

    Traditionally, aeropropulsion structural performance and aerodynamic performance have been designed separately and later mated together via flight testing. In today`s atmosphere of declining resources, it is imperative that more productive ways of designing and verifying aeropropulsion performance and structural interaction be made available to the aerospace industry. One method of obtaining a more productive design and evaluation capability is through the use of numerical simulations. Currently, Lawrence Livermore National Laboratory has developed a generalized fluid/structural interaction code known as ALE3D. This code is capable of characterizing fluid and structural interaction for components such as the combustor, fan/stators, inlet and/or nozzles. This code solves the 3D Euler equations and has been applied to several aeropropulsion applications such as a supersonic inlet and a combustor rupture simulation. To characterize aerodynamic-structural interaction for rotating components such as the compressor, appropriate turbomachinery simulations would need to be implemented within the ALE3D structure. The Arnold Engineering Development Center is currently developing a three-dimensional compression system code known as TEACC (Turbine Engine Analysis Compressor Code). TEACC also solves the 3D Euler equations and is intended to simulate dynamic behavior such as inlet distortion, surge or rotating stall. The technology being developed within the TEACC effort provides the necessary turbomachinery simulation for implementation into ALE3D. This paper describes a methodology to combine three-dimensional aerodynamic turbomachinery technology into the existing aerodynamic-structural interaction simulation, ALE3D to obtain the desired aerodynamic and structural integrated simulation for an aeropropulsion system.

  16. Aerodynamic Design Criteria for Class 8 Heavy Vehicles Trailer Base Devices to Attain Optimum Performance

    SciTech Connect (OSTI)

    Salari, K; Ortega, J

    2010-12-13

    Lawrence Livermore National Laboratory (LLNL) as part of its Department of Energy (DOE), Energy Efficiency and Renewable Energy (EERE), and Vehicle Technologies Program (VTP) effort has investigated class 8 tractor-trailer aerodynamics for many years. This effort has identified many drag producing flow structures around the heavy vehicles and also has designed and tested many new active and passive drag reduction techniques and concepts for significant on the road fuel economy improvements. As part of this effort a database of experimental, computational, and conceptual design for aerodynamic drag reduction devices has been established. The objective of this report is to provide design guidance for trailer base devices to improve their aerodynamic performance. These devices are commonly referred to as boattails, base flaps, tail devices, and etc. The information provided here is based on past research and our most recent full-scale experimental investigations in collaboration with Navistar Inc. Additional supporting data from LLNL/Navistar wind tunnel, track test, and on the road test will be published soon. The trailer base devices can be identified by 4 flat panels that are attached to the rear edges of the trailer base to form a closed cavity. These devices have been engineered in many different forms such as, inflatable and non-inflatable, 3 and 4-sided, closed and open cavity, and etc. The following is an in-depth discussion with some recommendations, based on existing data and current research activities, of changes that could be made to these devices to improve their aerodynamic performance. There are 6 primary factors that could influence the aerodynamic performance of trailer base devices: (1) Deflection angle; (2) Boattail length; (3) Sealing of edges and corners; (4) 3 versus 4-sided, Position of the 4th plate; (5) Boattail vertical extension, Skirt - boattail transition; and (6) Closed versus open cavity.

  17. Diameter of the NEPS of Bipartite Graphs Richard A. Brualdi and Jian Shen y

    E-Print Network [OSTI]

    Brualdi, Richard A.

    Diameter of the NEPS of Bipartite Graphs Richard A. Brualdi #3; and Jian Shen y Department 4, 2000 Abstract We prove that, if connected, the NEPS of connected, bipartite graphs has diameter-complete, extended p-sum, abbreviated NEPS, of G 1 ; G 2 ; : : : ; G n with basis B is the graph (see e.g. [1]) G

  18. Relating Airway Diameter Distributions to Regular Branching Asymmetry in the Lung Arnab Majumdar,1,2

    E-Print Network [OSTI]

    Buldyrev, Sergey

    Relating Airway Diameter Distributions to Regular Branching Asymmetry in the Lung Arnab Majumdar,1 as a function of generation N in asymmetric airway trees of mammalian lungs. We find that the airway]. Most models of the lung airway tree either do not address the observed diameter heterogeneity or simply

  19. THE RADIO NUMBERS OF ALL GRAPHS OF ORDER n AND DIAMETER n -2

    E-Print Network [OSTI]

    Tomova, Maggy

    THE RADIO NUMBERS OF ALL GRAPHS OF ORDER n AND DIAMETER n - 2 KATHERINE BENSON, MATTHEW PORTER, AND MAGGY TOMOVA Abstract. A radio labeling of a connected graph G is a function c : V (G) Z+ such that for every two distinct vertices u and v of G distance(u, v) + |c(u) - c(v)| 1 + diameter(G). The radio

  20. The Syntenic Diameter of the Space of N-Chromosome Genomes Jon Kleinberg

    E-Print Network [OSTI]

    Liben-Nowell, David

    The Syntenic Diameter of the Space of N-Chromosome Genomes Jon Kleinberg Department of Computer genomes of different species. For each of these measures, a natu- ral but often difficult problem is to determine the diameter of the space it defines: What is the maximum distance between any pair of genomes

  1. The Syntenic Diameter of the Space of NChromosome Genomes # Jon Kleinberg

    E-Print Network [OSTI]

    Liben-Nowell, David

    The Syntenic Diameter of the Space of N­Chromosome Genomes # Jon Kleinberg Department of Computer genomes of di#erent species. For each of these measures, a natu­ ral but often di#cult problem is to determine the diameter of the space it defines: What is the maximum distance between any pair of genomes

  2. Aerodynamic force measurement on a large-scale model in a short duration test facility

    SciTech Connect (OSTI)

    Tanno, H.; Kodera, M.; Komuro, T.; Sato, K.; Takahasi, M.; Itoh, K.

    2005-03-01

    A force measurement technique has been developed for large-scale aerodynamic models with a short test time. The technique is based on direct acceleration measurements, with miniature accelerometers mounted on a test model suspended by wires. Measuring acceleration at two different locations, the technique can eliminate oscillations from natural vibration of the model. The technique was used for drag force measurements on a 3 m long supersonic combustor model in the HIEST free-piston driven shock tunnel. A time resolution of 350 {mu}s is guaranteed during measurements, whose resolution is enough for ms order test time in HIEST. To evaluate measurement reliability and accuracy, measured values were compared with results from a three-dimensional Navier-Stokes numerical simulation. The difference between measured values and numerical simulation values was less than 5%. We conclude that this measurement technique is sufficiently reliable for measuring aerodynamic force within test durations of 1 ms.

  3. Stochastic model for aerodynamic force dynamics on wind turbine blades in unsteady wind inflow

    E-Print Network [OSTI]

    Luhur, Muhammad Ramzan; Khn, Martin; Wchter, Matthias

    2015-01-01

    The paper presents a stochastic approach to estimate the aerodynamic forces with local dynamics on wind turbine blades in unsteady wind inflow. This is done by integrating a stochastic model of lift and drag dynamics for an airfoil into the aerodynamic simulation software AeroDyn. The model is added as an alternative to the static table lookup approach in blade element momentum (BEM) wake model used by AeroDyn. The stochastic forces are obtained for a rotor blade element using full field turbulence simulated wind data input and compared with the classical BEM and dynamic stall models for identical conditions. The comparison shows that the stochastic model generates additional extended dynamic response in terms of local force fluctuations. Further, the comparison of statistics between the classical BEM, dynamic stall and stochastic models' results in terms of their increment probability density functions gives consistent results.

  4. Sand transverse dune aerodynamics: 3D Coherent Flow Structures from a computational study

    E-Print Network [OSTI]

    Bruno, Luca

    2015-01-01

    The engineering interest about dune fields is dictated by the their interaction with a number of human infrastructures in arid environments. The aerodynamic behaviour of sand dunes in atmospheric boundary layer belongs to the class of bluff bodies. Because of their simple geometry and their frequent occurrence in desert area, transverse sand dunes are usually adopted in literature as a benchmark to investigate dune aerodynamics by means of both computational or experimental approach, usually in nominally 2D setups. The writers suspect the flow in the wake is characterised by 3D features and affected by wind tunnel setup - e.g. blockage effect, duct side wall boundary layer, incoming velocity profile - when experimental studies are carried out. The present study aims at evaluating the 3D flow features of an idealised transverse dune under different setup conditions by means of computational simulations and to compare the obtained results with experimental measurements.

  5. Progress in Reducing Aerodynamic Drag for Higher Efficiency of Heavy Duty Trucks (Class 7-8)

    SciTech Connect (OSTI)

    Rose McCallen; Richard Couch; Juliana Hsu; Fred Browand; Mustapha Hammache; Anthony Leonard; Mark Brady; Kambiz Salari; Walter Rutledge; James Ross; Bruce Storms; J.T. Heineck; David Driver; James Bell; Gregory Zilliac

    1999-12-31

    This paper describes research and development for reducing the aerodynamic drag of heavy vehicles by demonstrating new approaches for the numerical simulation and analysis of aerodynamic flow. In addition, greater use of newly developed computational tools holds promise for reducing the number of prototype tests, for cutting manufacturing costs, and for reducing overall time to market. Experimental verification and validation of new computational fluid dynamics methods are also an important part of this approach. Experiments on a model of an integrated tractor-trailer are underway at NASA Ames Research Center and the University of Southern California. Companion computer simulations are being performed by Sandia National Laboratories, Lawrence Livermore National Laboratory, and California Institute of Technology using state-of-the-art techniques, with the intention of implementing more complex methods in the future.

  6. FY 2004 Annual Report: DOE Project on Heavy Vehicle Aerodynamic Drag

    SciTech Connect (OSTI)

    McCallen, R C; Salari, K; Ortega, J; Castellucci, P; Eastwood, C; Whittaker, K; DeChant, L J; Roy, C J; Payne, J L; Hassan, B; Pointer, W D; Browand, F; Hammache, M; Hsu, T; Ross, J; Satran, D; Heineck, J T; Walker, S; Yaste, D; Englar, R; Leonard, A; Rubel, M; Chatelain, P

    2004-11-18

    The objective of this report is: (1) Provide guidance to industry in the reduction of aerodynamic drag of heavy truck vehicles; and (2) Establish a database of experimental, computational, and conceptual design information, and demonstrate potential of new drag-reduction devices. The approaches used were: (1) Develop and demonstrate the ability to simulate and analyze aerodynamic flow around heavy truck vehicles using existing and advanced computational fluid dynamics (CFD) tools; (2) Through an extensive experimental effort, generate an experimental data base for code validation; (3) Using experimental data base, validate computations; (4) Provide industry with design guidance and insight into flow phenomena from experiments and computations; and (5) Investigate aero devices (e.g., base flaps, tractor-trailer gap stabilizer, underbody skirts and wedges, blowing and acoustic devices), provide industry with conceptual designs of drag reducing devices, and demonstrate the full-scale fuel economy potential of these devices.

  7. DOE Project on Heavy Vehicle Aerodynamic Drag FY 2005 Annual Report

    SciTech Connect (OSTI)

    McCallen, R C; Salari, K; Ortega, J; Castellucci, P; Eastwood, C; Paschkewitz, J; Pointer, W D; DeChant, L J; Hassan, B; Browand, F; Radovich, C; Merzel, T; Plocher, D; Ross, J; Storms, B; Heineck, J T; Walker, S; Roy, C J

    2005-11-14

    Class 8 tractor-trailers consume 11-12% of the total US petroleum use. At high way speeds, 65% of the energy expenditure for a Class 8 truck is in overcoming aerodynamic drag. The project objective is to improve fuel economy of Class 8 tractor-trailers by providing guidance on methods of reducing drag by at least 25%. A 25% reduction in drag would present a 12% improvement in fuel economy at highway speeds, equivalent to about 130 midsize tanker ships per year. Specific goals include: (1) Provide guidance to industry in the reduction of aerodynamic drag of heavy truck vehicles; and (2) Establish a database of experimental, computational, and conceptual design information, and demonstrate the potential of new drag-reduction devices.

  8. July 2004 Working Group Meeting on Heavy Vehicle Aerodynamic Drag: Presentation, Summary of Comments, and Conclusions

    SciTech Connect (OSTI)

    McCallen, R; Salari, K; Ortega, J; Castellucci, P; Eastwood, C; DeChant, L; Hassan, B; Browand, F; Arcas, D; Ross, J; Heineck, J; Storms, B; Walker, S; Leonard, A; Roy, C; Whitfield, D; Pointer, D; Sofu, T; Englar, R; Funk, R

    2004-08-17

    A Working Group Meeting on Heavy Vehicle Aerodynamic Drag was held in Portland, Oregon on July 1, 2004. The purpose of the meeting was to provide a summary of achievements, discuss pressing issues, present a general overview of future plans, and to provide a forum for dialogue with the Department of Energy (DOE) and industry representatives. The meeting was held in Portland, because the DOE Aero Team participated in an exclusive session on Heavy Truck Vehicle Aerodynamic Drag at the 34th AIAA Fluid Dynamics Conference and Exhibit in Portland on the morning of July 1st, just preceding our Working Group meeting. Even though the paper session was on the last day of the Conference, the Team presented to a full room of interested attendees.

  9. Aerodynamic Models For Hurricanes I. Model description and horizontal motion of hurricane

    E-Print Network [OSTI]

    Leonov, Arkady I

    2008-01-01

    Aerodynamic models are developed to describe coherent structures and transport processes in hurricanes moving over open seas. The models consist of the lower boundary layer and upper adiabatic layer. Except friction at the air/sea interface,proposed modeling avoids the common turbulent approximations while using explicitly or implicitly basic stability constraints. The models analyze dynamics of upper hurricane adiabatic layer, dynamics and transport processes in hurricane boundary layer, and genesis and maturing of hurricane. The proposed modeling provides a rude enough but consistent analytical description of basic processes in hurricanes. The present paper qualitatively describes the model of mature hurricane, briefly discusses the basic thermodynamic relations and aerodynamic equations, and establishes the principles of horizontal motion for mature hurricane.

  10. DOE's effort to reduce truck aerodynamic drag : joint experiments and computations lead to smart design.

    SciTech Connect (OSTI)

    Yaste, David M (NASA Ames Research Center, Moffet Field, CA); Salari, Kambiz (Lawrence Livermore National Laboratory, Livermore, CA); Hammache, Mustapha (University of Southern California, Los Angeles, CA); Browand, Fred (University of Southern California, Los Angeles, CA); Pointer, W. David (Argonne National Laboratory, Argonne, IL); Ortega, Jason M. (Lawrence Livermore National Laboratory, Livermore, CA); McCallen, Rose (Lawrence Livermore National Laboratory, Livermore, CA); Walker, Stephen M (NASA Ames Research Center, Moffet Field, CA); Heineck, James T (NASA Ames Research Center, Moffet Field, CA); Hassan, Basil; Roy, Christopher John (Auburn University, Auburn, AL); Storms, B. (NASA Ames Research Center, Moffet Field, CA); Satran, D. (NASA Ames Research Center, Moffet Field, CA); Ross, James (NASA Ames Research Center, Moffet Field, CA); Englar, Robert (Georgia Tech Research Institute, Atlanta, GA); Chatalain, Philippe (Caltech, Pasadena, CA); Rubel, Mike (Caltech, Pasadena, CA); Leonard, Anthony (Caltech, Pasadena, CA); Hsu, Tsu-Ya (University of Southern California, Los Angeles, CA); DeChant, Lawrence Justin.

    2004-06-01

    At 70 miles per hour, overcoming aerodynamic drag represents about 65% of the total energy expenditure for a typical heavy truck vehicle. The goal of this US Department of Energy supported consortium is to establish a clear understanding of the drag producing flow phenomena. This is being accomplished through joint experiments and computations, leading to the smart design of drag reducing devices. This paper will describe our objective and approach, provide an overview of our efforts and accomplishments, and discuss our future direction.

  11. DOE's Effort to Reduce Truck Aerodynamic Drag-Joint Experiments and Computations Lead to Smart Design

    SciTech Connect (OSTI)

    McCallen, R; Salari, K; Ortega, J; DeChant, L; Hassan, B; Roy, C; Pointer, W; Browand, F; Hammache, M; Hsu, T; Leonard, A; Rubel, M; Chatalain, P; Englar, R; Ross, J; Satran, D; Heineck, J; Walker, S; Yaste, D; Storms, B

    2004-06-17

    At 70 miles per hour, overcoming aerodynamic drag represents about 65% of the total energy expenditure for a typical heavy truck vehicle. The goal of this US Department of Energy supported consortium is to establish a clear understanding of the drag producing flow phenomena. This is being accomplished through joint experiments and computations, leading to the 'smart' design of drag reducing devices. This paper will describe our objective and approach, provide an overview of our efforts and accomplishments, and discuss our future direction.

  12. Working group meeting on heavy vehicle aerodynamic drag: presentations and summary of comments and conclusion

    SciTech Connect (OSTI)

    Browand, F; Gutierrez, W; Leonard, A; McBride, D; McCallen, R; Ross, J; Roth, K; Rutledge, W; Salari, K

    1998-09-28

    The first Working Group Meeting on Heavy Vehicle Aerodynamic Drag was held at Sandia National Laboratories (SNL) in Albuquerque, New Mexico on August 28, 1998. The purpose of the meeting was to review the proposed Multi-Year Program Plan (MYPP) and provide an update on the Group"s progress. In addition, the technical details of each organization"s activities were presented and discussed. Presentations were given by representatives from the Department of Energy (DOE) Office of Transportation Technology Office of Heavy Vehicle Technology (OHVT), Lawrence Livermore National Laboratory (LLNL), SNL, University of Southern California (USC), California Institute of Technology (Caltech), and NASA Ames Research Center. These presenters are part of a DOE appointed Technical Team assigned to developing the MYPP. The goal of the MYPP is to develop and demonstrate the ability to simulate and analyze aerodynamic flow around heavy truck vehicles using existing and advanced computational tools (A Multi-Year Program Plan for the Aerodynamic Design of Heavy Vehicles, R. McCallen, D. McBride, W. Rutledge, F. Browand, A. Leonard, .I. Ross, UCRL-PROP- 127753 Dr. Rev 2, May 1998). This report contains the technical presentations (viewgraphs) delivered at the Meeting, briefly summarizes the comments and conclusions from the Meeting participants, and outlines the future actions.

  13. A Multi-Year Program Plan for the Aerodynamic Design of Heavy Vehicles

    SciTech Connect (OSTI)

    None

    2001-09-01

    The project tasks and deliverables are as follows: Computations and Experiments--(1) Simulation and analysis of a range of generic shapes, simplified to more complex, representative of tractor and integrated tractor-trailer flow characteristics using computational tools, (2) The establishment of an experimental data base for tractor-trailer models for code/computational method development and validation. The first shapes to be considered will be directed towards the investigation of tractor-trailer gaps and mismatch of tractor-trailer heights. (3) The evaluation and documentation of effective computational approaches for application to heavy vehicle aerodynamics based on the benchmark results with existing and advanced computational tools compared to experimental data, and (4) Computational tools and experimental methods for use by industry, National Laboratories, and universities for the aerodynamic modeling of heavy truck vehicles. Evaluation of current and new technologies--(1) The evaluation and documentation of current and new technologies for drag reduction based on published literature and continued communication with the heavy vehicle industry (e.g., identification and prioritization of tractor-trailer drag-sources, blowing and/or suction devices, body shaping, new experimental methods or facilities), and the identification and analysis of tractor and integrated tractor-trailer aerodynamic problem areas and possible solution strategies. (2) Continued industrial site visits. It should be noted that ''CFD tools'' are not only the actual computer codes, but descriptions of appropriate numerical solution methods. Part of the project effort will be to determine the restrictions or avenues for technology transfer.

  14. Working group meeting on heavy vehicle aerodynamic drag: presentations and summary of comments and

    SciTech Connect (OSTI)

    Browand, F; Gutierrez, W; Leonard, A; McBride, D; McCallen, R; Ross, J; Roth, K; Rutledge, W; Salari, K.

    1998-09-28

    The first Working Group Meeting on Heavy Vehicle Aerodynamic Drag was held at Sandia National Laboratories (SNL) in Albuquerque, New Mexico on August 28, 1998. The purpose of the meeting was to review the proposed Multi-Year Program Plan (MYPP) and provide an update on the Group s progress. In addition, the technical details of each organization s activities were presented and discussed. Presentations were given by representatives from the Department of Energy (DOE) Office of Transportation Technology Office of Heavy Vehicle Technology (OHVT), Lawrence Livermore National Laboratory (LLNL), SNL, University of Southern California (USC), California Institute of Technology (Caltech), and NASA Ames Research Center. These presenters are part of a DOE appointed Technical Team assigned to developing the MYPP. The goal of the MYPP is to develop and demonstrate the ability to simulate and analyze aerodynamic flow around heavy truck vehicles using existing and advanced computational tools (A Multi-Year Program Plan for the Aerodynamic Design of Heavy Vehicles, R. McCallen, D. McBride, W. Rutledge, F. Browand, A. Leonard, .I. Ross, UCRL-PROP- 127753 Dr. Rev 2, May 1998). This report contains the technical presentations (viewgraphs) delivered at the Meeting, briefly summarizes the comments and conclusions from the Meeting participants, and outlines the future actions.

  15. Effect of flow rate on clogging processes in small diameter aquifer storage and recovery injection wells

    E-Print Network [OSTI]

    Thompson, Angela R.

    2014-12-31

    (KGS) investigates a low-cost, slow flow alternative to traditional ASR recharge systems. The project utilizes gravity-induced recharge and small diameter wells installed with direct-push technology to recharge and store ground water. The KGS ASR...

  16. Diameters of delta Cephei and eta Aquilae Measured with the Navy Prototype Optical Interferometer

    E-Print Network [OSTI]

    J. T. Armstrong; Tyler E. Nordgren; M. E. Germain; Arsen R. Hajian; R. B. Hindsley; C. A. Hummel; D. Mozurkewich; R. N. Thessin

    2000-09-25

    We have measured the diameters of the Cepheid variables delta Cephei (18 nights) and eta Aquilae (11 nights) with the Navy Prototype Optical Interferometer. The primary results of these observations are the mean angular diameters of these Cepheids: 1.520 +/- 0.014 milliseconds of arc (mas) for delta Cep and 1.69 +/- 0.04 mas for eta Aql. We also report limb-darkened diameters for the check stars in this program: for beta Lac, theta(LD) = 1.909 +/- 0.011 mas, and for 12 Aql, theta(LD) = 2.418 +/- 0.010 mas. When combined with radius estimates from period-radius relations in the literature, the Cepheid angular diameters suggest distances slightly smaller than, but still consistent with, the Hipparcos distances. Pulsations are weakly detected at a level of about 1.5 sigma to 2 sigma for both Cepheids.

  17. Flooding Experiments with Steam and Water in a Large Diameter Vertical Tube

    E-Print Network [OSTI]

    Williams, Susan Nicole

    2010-10-12

    An experimental study on flooding with steam and water in a large diameter vertical tube was conducted. This research has been performed to provide a better prediction of flooding in a pressurized water reactor (PWR) ...

  18. Handling state-of-the-art large-diameter coiled tubing

    SciTech Connect (OSTI)

    Courville, P.

    1994-12-31

    Completion and workover demands placed on coiled tubing technology in the last 10 years have shown the limitations of small-diameter (1- to 1{1/2}-in.) coiled tubing. The small tubing tends to buckle when used at lengths greater than 1,500 ft in most horizontal applications. Large-diameter coiled tubing (up to 3{1/2} in.) provides greater flexibility of job design and increases horizontal reach possibilities for drilling, completion, and workover activities. Transportation and handling equipment to accommodate the larger, heavier tubing is naturally a critical component of the system. This paper will present the benefits of large-diameter coiled tubing including completion and workover for greater depth and more extended horizontal reach. It will also discuss the unique concerns of transportation and handling of large diameter tubing and associated equipment.

  19. (lOpts) 1. An inverted conical tank whose diameter is 8 In and height ...

    E-Print Network [OSTI]

    (lOpts) 1. An inverted conical tank whose diameter is 8 In and height 10 n1 contains crude oil that is leaking out the bottom at a rate of 5 m3 / hr. How fast is the...

  20. The effects of inlet velocity and barrel diameter on cyclone performance

    E-Print Network [OSTI]

    Faulkner, William Brock

    2006-08-16

    ) of the entrained aerosol. Multiple models have been proposed to predict the performance of cyclones given different geometric proportions, but many of these models do not quantify changes in performance with changes in inlet velocity or cyclone diameter given fixed...

  1. Economic feasibility of products from inland west small-diameter timber. Forest Service general technical report

    SciTech Connect (OSTI)

    Spelter, H.; Wang, R.; Ince, P.

    1996-05-01

    A large part of the forests located in the Rocky Mountain region of the U.S. West (inland West) is characterized by densely packed, small-diameter stands. The purpose of this study was to examine the economic feasibility of using small-diameter material from this resource to manufacture various wood products: oriented strandboard (OSB), stud lumber, random-length dimension lumber, machine-stress-rated random-length lumber, laminated veneer lumber (LVL), and market pulp.

  2. INTEGR. COMP. BIOL., 42:10091017 (2002) Experimental Hydrodynamics and Evolution: Function of Median Fins in Ray-finned Fishes1

    E-Print Network [OSTI]

    Lauder, George V.

    2002-01-01

    . But the orientations and magnitudes of these forces, the mechanisms by which they are generated, and how fish modulate reveal that lateral forces are high relative to thrust force, and that mechanical performance of median propulsor may also enhance stability and maneuverability. Analysis of hydrodynamic function of the soft

  3. Diffusive Shock Acceleration of Electrons and Radio Emission from Large Diameter Shell-Type Supernova Remnants

    E-Print Network [OSTI]

    A. I. Asvarov

    2000-01-21

    In present study I examine the capability of diffusive shock acceleration mechanism to explain existing data on radio emission from evolved large diameter shell-type adiabatic supernova remnants (SNRs). Time-dependent ''onion-shell'' model for the radio emission of SNRs is developed, which is based on the assumptions: a) acceleration takes place from thermal energies and test-particle approximation is valid; b) the problem of injection is avoided by introducing, like Bell (1978), two injection parameters; c) to take into consideration very late stages of SNR evolution the analytic approximation of Cox and Andersen (1982) for the shell structure is used; c)no radiative cooling. Constructed Surface Brightness - Diameter $(\\Sigma -D)$ tracks are compared with the empirical $\\Sigma -D$ diagram. The main conclusion of the study is that the DSA mechanism is capable of explaining all the statistics of radio SNRs including very large diameter remnants and giant galactic loops.

  4. Large Diameter Limbs for Dilated Common Iliac Arteries in Endovascular Aneurysm Repair. Is It Safe?

    SciTech Connect (OSTI)

    Malagari, Katerina Brountzos, Elias; Gougoulakis, Alexandros; Papathanasiou, Matilda; Alexopoulou, Efthymia; Mastorakou, Renata; Kelekis, Dimitris

    2004-09-15

    In this prospective study we examined whether dilated common iliac arteries (CIAs) can provide a safe distal seal in endovascular aneurysm repair (EVAR) with the use of bifurcated stent grafts with large diameter limbs. Sixteen patients with 26 dilated CIAs with a diameter of {>=}6 mm who were offered EVAR using stent grafts with large diameter limbs were included in the study (Group A). Forty-two patients who also underwent EVAR without iliac dilatation, matched for age, sex and surgical risk were used for comparison (controls-Group B). In group A mean CIA diameter was 18.2 mm (16-28) and mean abdominal aortic aneurysm (AAA) diameter was 6.87 {+-} 1.05 cm; mean age was 77.2 {+-} 4.8 yrs (67-81). Mean follow-up was 33.6 months (2.8 yrs). CIA diameter changes and development of endoleaks were assessed by CT angiography (CTA). Overall iliac dilatation was present in 16/58 of our patients (27.6%). In 10 patients dilatation was bilateral (17.3%). Partial or complete flow to the internal iliac artery (IIA) territories was preserved in all patients post-EVAR. On follow-up, stable caliber of the dilated CIAs was observed in 21 patients (84%), enlargement of 1mm in 3 (16%), and failure of the distal attachment in 1 (6.2%). Compared to the control group there was no statistical significance in the incidence of complications. Dilated common iliac arteries provide a safe distal seal in patients who have undergone EVAR, thus obviating the need for additional endovascular procedures and sparing flow in the IIA vascular bed.

  5. Development of Pneumatic Aerodynamic Devices to Improve the Performance, Economics, and Safety of Heavy Vehicles

    SciTech Connect (OSTI)

    Robert J. Englar

    2000-06-19

    Under contract to the DOE Office of Heavy Vehicle Technologies, the Georgia Tech Research Institute (GTRI) is developing and evaluating pneumatic (blown) aerodynamic devices to improve the performance, economics, stability and safety of operation of Heavy Vehicles. The objective of this program is to apply the pneumatic aerodynamic aircraft technology previously developed and flight-tested by GTRI personnel to the design of an efficient blown tractor-trailer configuration. Recent experimental results obtained by GTRI using blowing have shown drag reductions of 35% on a streamlined automobile wind-tunnel model. Also measured were lift or down-load increases of 100-150% and the ability to control aerodynamic moments about all 3 axes without any moving control surfaces. Similar drag reductions yielded by blowing on bluff afterbody trailers in current US trucking fleet operations are anticipated to reduce yearly fuel consumption by more than 1.2 billion gallons, while even further reduction is possible using pneumatic lift to reduce tire rolling resistance. Conversely, increased drag and down force generated instantaneously by blowing can greatly increase braking characteristics and control in wet/icy weather due to effective ''weight'' increases on the tires. Safety is also enhanced by controlling side loads and moments caused on these Heavy Vehicles by winds, gusts and other vehicles passing. This may also help to eliminate the jack-knifing problem if caused by extreme wind side loads on the trailer. Lastly, reduction of the turbulent wake behind the trailer can reduce splash and spray patterns and rough air being experienced by following vehicles. To be presented by GTRI in this paper will be results developed during the early portion of this effort, including a preliminary systems study, CFD prediction of the blown flowfields, and design of the baseline conventional tractor-trailer model and the pneumatic wind-tunnel model.

  6. Structure of Nup58/45 Suggests Flexible Nuclear Pore Diameter by Intermolecular Sliding

    SciTech Connect (OSTI)

    Melcak,I.; Hoelz, A.; Blobel, G.

    2007-01-01

    The nucleoporins Nup58 and Nup45 are part of the central transport channel of the nuclear pore complex, which is thought to have a flexible diameter. In the crystal structure of an {alpha}-helical region of mammalian Nup58/45, we identified distinct tetramers, each consisting of two antiparallel hairpin dimers. The intradimeric interface is hydrophobic, whereas dimer-dimer association occurs through large hydrophilic residues. These residues are laterally displaced in various tetramer conformations, which suggests an intermolecular sliding by 11 angstroms. We propose that circumferential sliding plays a role in adjusting the diameter of the central transport channel.

  7. Aerodynamics overview of the ground transportation systems (GTS) project for heavy vehicle drag reduction

    SciTech Connect (OSTI)

    Gutierrez, W.T.; Hassan, B.; Croll, R.H.; Rutledge, W.H.

    1995-12-31

    The focus of the research was to investigate the fundamental aerodynamics of the base flow of a tractor trailer that would prove useful in fluid flow management. Initially, industry design needs and constraints were defined. This was followed by an evaluation of state-of-the-art Navier-Stokes based computational fluid dynamics tools. Analytical methods were then used in combination with computational tools in a design process. Several geometries were tested at 1:8 scale in a low speed wind tunnel. In addition to the baseline geometry, base add-on devices of the class of ogival boattails and slants were analyzed.

  8. Systematic approach to analyzing and reducing aerodynamic drag of heavy vehicles

    SciTech Connect (OSTI)

    McCallen, R.; Browand, F.; Leonard, A.; Rutledge, W.

    1997-09-16

    This paper presents an approach for reducing aerodynamic drag of heavy vehicles by systematically analyzing trailer components using existing computational tools and moving on to the analyses of integrated tractor-trailers using advanced computational tools. Experimental verification and validation are also an important part of this approach. The project is currently in the development phase while we are in the process of constructing a Multi-Year Program Plan. Projects I and 2 as described in this paper are the anticipated project direction. Also included are results from past and current related activities by the project participants which demonstrate the analysis approach.

  9. Aerodynamic Models for Hurricanes II. Model of the upper hurricane layer

    E-Print Network [OSTI]

    Leonov, Arkady I

    2008-01-01

    This second paper of the series (see the first one in [1]) models the dynamics and structure of upper hurricane layer in adiabatic approximation. Formulation of simplified aerodynamic model allows analytically express the radial istributions of pressure and wind speed components. The vertical evolution of these distributions and hurricane structure in the layer are described by a coupled set of equations for the vertical mass flux and vertical momentum balance, averaged over the eye wall cross section. Several realistic predictions of the model are demonstrated, including the change of directions for the component of radial wind speed and angular velocity of hurricane with altitude.

  10. Cavitation as a complementary tool for automotive aerodynamics J.F. Beaudoin, O. Cadot, J.L. Aider, K. Gosse, P. Paranthoen, B. Hamelin,

    E-Print Network [OSTI]

    Wesfreid, Jos Eduardo

    Cavitation as a complementary tool for automotive aerodynamics J.F. Beaudoin, O. Cadot, J.L. Aider of this pollution is related to the increasing number of road vehicles and their gas emissions. For the automotive with a variable slant angle. As depicted in Fig. 1, it exhibits the main features of automotive aerodynamics

  11. The Variability of LateType Stars' Diameters Measured Using MidInfrared Interferometry

    E-Print Network [OSTI]

    California at Berkeley, University of

    in temperature within the star are exaggerated in the visible and a non­uniform intensity distribution to the diameter of a main­sequence star like the sun. The sun is observed to be a bright circular disk with a well several hundred times that of the sun, with comparable masses in some cases. As a consequence

  12. Diameter-Controlled and Nitrogen-Doped Vertically Aligned Single-Walled Carbon Theerapol Thurakitsereea

    E-Print Network [OSTI]

    Maruyama, Shigeo

    ], methane [8], acetylene [9], ethylene [10], or other organic chemical sources [11]. Acetonitrile (CH3CN SWCNT by no-flow chemical vapor deposition (CVD) from Co/Mo binary catalyst. The mean diameters). The process is based on that described in Ref. [23]. During heating of the CVD system, the Co/Mo binary

  13. Subcooling Effects for Flooding Experiments with Steam and Water in a Large Diameter Vertical Tube

    E-Print Network [OSTI]

    Cullum, Wes

    2012-10-19

    rate needed to induce flooding. The data more closely follow air-water data at low subcooling. Such data has not been seen in the literature for steam-water flooding experiments in a large diameter vertical tube and will serve as an important benchmark....

  14. Carbon nanotube diameter selection by pretreatment of metal catalysts on surfaces

    DOE Patents [OSTI]

    Hauge, Robert H. (Houston, TX); Xu, Ya-Qiong (Houston, TX); Shan, Hongwei (Houston, TX); Nicholas, Nolan Walker (South Charleston, WV); Kim, Myung Jong (Houston, TX); Schmidt, Howard K. (Cypress, TX); Kittrell, W. Carter (Houston, TX)

    2012-02-28

    A new and useful nanotube growth substrate conditioning processes is herein disclosed that allows the growth of vertical arrays of carbon nanotubes where the average diameter of the nanotubes can be selected and/or controlled as compared to the prior art.

  15. Implementation and evaluation of prognostic representations of the optical diameter of snow in the

    E-Print Network [OSTI]

    Implementation and evaluation of prognostic representations of the optical diameter of snow Grenoble 1, LGGE, Grenoble, France A good representation of snow metamorphism processes within snowpack models is crucial, since the characteristics of snow grains have a significant impact on many

  16. Anomalous diameter dependence of thermal transport in ultra-narrow Si nanowires

    SciTech Connect (OSTI)

    Karamitaheri, Hossein, E-mail: karami@iue.tuwien.ac.at [Institute for Microelectronics, TU Wien, Guhausstrae 27-29/E360, A-1040 Wien (Austria); Department of Electrical Engineering, University of Kashan, Kashan, 87317-51167 (Iran, Islamic Republic of); Neophytou, Neophytos, E-mail: neophytou@iue.tuwien.ac.at [Institute for Microelectronics, TU Wien, Guhausstrae 27-29/E360, A-1040 Wien (Austria); School of Engineering, University of Warwick, Coventry CV4 7AL (United Kingdom); Kosina, Hans, E-mail: kosina@iue.tuwien.ac.at [Institute for Microelectronics, TU Wien, Guhausstrae 27-29/E360, A-1040 Wien (Austria)

    2014-01-14

    We present atomistic valence force field calculations of thermal transport in Si nanowires of diameters from 12?nm down to 1?nm. We show that as the diameter is reduced, the phonon density-of-states and transmission function acquire a finite value at low frequency, in contrast to approaching zero as in the bulk material. It turns out that this effect results in what Ziman described as the problem of long longitudinal waves [J. M. Ziman, Electrons and Phonons: The Theory of Transport Phenomena in Solids (Clarendon, Oxford, 1962)], which states that the thermal conductivity of a material increases as its length is increased due to the vanishing scattering for long-wavelength phonons. We show that this thermal transport improvement also appears in nanowires as their diameter is decreased below D?=?5?nm (not only as the length increases), originating from the increase in the density of the long wavevector modes. The observation is present under ballistic transport conditions, and further enhanced with the introduction of phonon-phonon scattering. Because of this, in such ultra-narrow nanowires, as the diameter is reduced, phonon transport is dominated more and more by lower energy phonons with longer mean-free paths. We show that ?80% of the heat is carried by phonons with energies less than 5?meV, most with mean-free paths of several hundreds of nanometers.

  17. Growth and field emission properties of small diameter carbon nanotube films

    E-Print Network [OSTI]

    Qin, Lu-Chang

    Growth and field emission properties of small diameter carbon nanotube films Y.Y. Wanga,*, S are comprised of both single- and double-wall nanotubes. The electron field emission properties of the films were investigated by variable distance field emission and temperature-dependent field electron emission

  18. Single-Walled Carbon Nanotubes of Controlled Diameter and Bundle Size and Their Field Emission Properties

    E-Print Network [OSTI]

    Resasco, Daniel

    Single-Walled Carbon Nanotubes of Controlled Diameter and Bundle Size and Their Field Emission: June 8, 2005 Field emission studies were conducted on as-produced CoMoCAT single-walled carbon nanotube became larger, but the bundle size became smaller. A gradual and consistent reduction in the emission

  19. An evaluation of large diameter coiled tubing for subsurface production tubulars

    SciTech Connect (OSTI)

    Adams, L.S.; Smith, L.W.

    1995-12-31

    This paper provides an economic and technological perspective for use of large diameter coiled tubing relative to threaded tubulars for subsurface production tubing. This new advancement in coiled tubing technology can significantly reduce the expense for purchasing and installing production tubing while increasing hydrocarbon reserve recovery and providing a safer, more desirable ecosystem interrelation.

  20. Production of vertical arrays of small diameter single-walled carbon nanotubes

    DOE Patents [OSTI]

    Hauge, Robert H; Xu, Ya-Qiong

    2013-08-13

    A hot filament chemical vapor deposition method has been developed to grow at least one vertical single-walled carbon nanotube (SWNT). In general, various embodiments of the present invention disclose novel processes for growing and/or producing enhanced nanotube carpets with decreased diameters as compared to the prior art.

  1. Free-Air Performance Tests of a 5-Metre-Diameter Darrieus Turbine

    E-Print Network [OSTI]

    ABSTRACT A 5-metre - diameter vertical-axis wind turbine has been tested at the Sandia Laboratories Wind 5 6 7 8 9 10 11 12 FIGURES The Sandia 5- Metre Vertical Axis Wind Turbine at the Wind Turbine Site Turbine Site. The results of these tests and some of the problems associated with free-air testing of wind

  2. Atomic Layer Deposition to Fine-Tune the Surface Properties and Diameters of

    E-Print Network [OSTI]

    Atomic Layer Deposition to Fine-Tune the Surface Properties and Diameters of Fabricated Nanopores 02138 Received April 23, 2004; Revised Manuscript Received May 12, 2004 ABSTRACT Atomic layer deposition. The control over the chemical and physical nature of the pore surface provided by atomic layer deposition

  3. Prediction of tree diameter growth using quantile regression and mixed-effects models

    E-Print Network [OSTI]

    Cao, Quang V.

    of Oklahoma Health Sciences Center, Oklahoma City, OK 73104, USA b School of Renewable Natural ResourcesPrediction of tree diameter growth using quantile regression and mixed-effects models Som B. Bohora is an important component of an individual-tree model. This function can be considered as a mixed-effects model

  4. Hydraulics of a finite-diameter horizontal well with wellbore storage and skin effect

    E-Print Network [OSTI]

    Zhan, Hongbin

    Hydraulics of a finite-diameter horizontal well with wellbore storage and skin effect Eungyu Park, hydrogeologists have studied hydraulics of hori- zontal wells in shallow ground water aquifers [5,43,50 52 from the aquifer. Extensive studies on hydraulics of finite or large di- ameter vertical wells

  5. Centrifugal Pump for a 20-m/s, 1-cm-Diameter Mercury Jet

    E-Print Network [OSTI]

    McDonald, Kirk

    Centrifugal Pump for a 20-m/s, 1-cm-Diameter Mercury Jet Ernst de Haas, Kirk T. McDonald Joseph) centrifugal pump from R.S. Cor- coran, powered by a 20-hp, 480 V motor from Baldor. A photograph of this pump

  6. Coupling a Mesoscale Numerical Weather Prediction Model with Large-Eddy Simulation for Realistic Wind Plant Aerodynamics Simulations (Poster)

    SciTech Connect (OSTI)

    Draxl, C.; Churchfield, M.; Mirocha, J.; Lee, S.; Lundquist, J.; Michalakes, J.; Moriarty, P.; Purkayastha, A.; Sprague, M.; Vanderwende, B.

    2014-06-01

    Wind plant aerodynamics are influenced by a combination of microscale and mesoscale phenomena. Incorporating mesoscale atmospheric forcing (e.g., diurnal cycles and frontal passages) into wind plant simulations can lead to a more accurate representation of microscale flows, aerodynamics, and wind turbine/plant performance. Our goal is to couple a numerical weather prediction model that can represent mesoscale flow [specifically the Weather Research and Forecasting model] with a microscale LES model (OpenFOAM) that can predict microscale turbulence and wake losses.

  7. Aerodynamically induced radial forces in a centrifugal gas compressor: Part 2 -- Computational investigation

    SciTech Connect (OSTI)

    Flathers, M.B.; Bache, G.E.

    1999-10-01

    Radial loads and direction of a centrifugal gas compressor containing a high specific speed mixed flow impeller and a single tongue volute were determined both experimentally and computationally at both design and off-design conditions. The experimental methodology was developed in conjunction with a traditional ASME PTC-10 closed-loop test to determine radial load and direction. The experimental study is detailed in Part 1 of this paper (Moore and Flathers, 1998). The computational method employs a commercially available, fully three-dimensional viscous code to analyze the impeller and the volute interaction. An uncoupled scheme was initially used where the impeller and volute were analyzed as separate models using a common vaneless diffuser geometry. The two calculations were then repeated until the boundary conditions at a chosen location in the common vaneless diffuser were nearly the same. Subsequently, a coupled scheme was used where the entire stage geometry was analyzed in one calculation, thus eliminating the need for manual iteration of the two independent calculations. In addition to radial load and direction information, this computational procedure also provided aerodynamic stage performance. The effect of impeller front face and rear face cavities was also quantified. The paper will discuss computational procedures, including grid generation and boundary conditions, as well as comparisons of the various computational schemes to experiment. The results of this study will show the limitations and benefits of Computational Fluid Dynamics (CFD) for determination of radial load, direction, and aerodynamic stage performance.

  8. Advanced Aerodynamic Devices to Improve the Performance, Economics, Handling, and Safety of Heavy Vehicles

    SciTech Connect (OSTI)

    Robert J. Englar

    2001-05-14

    Research is being conducted at the Georgia Tech Research Institute (GTRI) to develop advanced aerodynamic devices to improve the performance, economics, stability, handling and safety of operation of Heavy Vehicles by using previously-developed and flight-tested pneumatic (blown) aircraft technology. Recent wind-tunnel investigations of a generic Heavy Vehicle model with blowing slots on both the leading and trailing edges of the trailer have been conducted under contract to the DOE Office of Heavy Vehicle Technologies. These experimental results show overall aerodynamic drag reductions on the Pneumatic Heavy Vehicle of 50% using only 1 psig blowing pressure in the plenums, and over 80% drag reductions if additional blowing air were available. Additionally, an increase in drag force for braking was confirmed by blowing different slots. Lift coefficient was increased for rolling resistance reduction by blowing only the top slot, while downforce was produced for traction increase by blowing only the bottom. Also, side force and yawing moment were generated on either side of the vehicle, and directional stability was restored by blowing the appropriate side slot. These experimental results and the predicted full-scale payoffs are presented in this paper, as is a discussion of additional applications to conventional commercial autos, buses, motor homes, and Sport Utility Vehicles.

  9. DOE's effort to reduce truck aerodynamic drag through joint experiments and computations.

    SciTech Connect (OSTI)

    Salari, Kambiz (Lawrence Livermore National Laboratory); Browand, Fred (University of Southern California); Sreenivas, Kidambi (University of Tennessee, Chattanooga); Pointer, W. David (Argonne National Laboratory); Taylor, Lafayette (University of Tennessee, Chattanooga); Pankajakshan, Ramesh (University of Tennessee, Chattanooga); Whitfield, David (University of Tennessee, Chattanooga); Plocher, Dennis (University of Southern California); Ortega, Jason M. (Lawrence Livermore National Laboratory); Merzel, Tai (University of Southern California); McCallen, Rose (Lawrence Livermore National Laboratory); Walker, Stephen M (NASA Ames Research Center); Heineck, James T (NASA Ames Research Center); Hassan, Basil; Roy, Christopher John (Auburn University); Storms, B. (NASA Ames Research Center); Ross, James (NASA Ames Research Center); Englar, Robert (Georgia Tech Research Institute); Rubel, Mike (Caltech); Leonard, Anthony (Caltech); Radovich, Charles (University of Southern California); Eastwood, Craig (Lawrence Livermore National Laboratory); Paschkewitz, John (Lawrence Livermore National Laboratory); Castellucci, Paul (Lawrence Livermore National Laboratory); DeChant, Lawrence Justin.

    2005-08-01

    Class 8 tractor-trailers are responsible for 11-12% of the total US consumption of petroleum. Overcoming aero drag represents 65% of energy expenditure at highway speeds. Most of the drag results from pressure differences and reducing highway speeds is very effective. The goal is to reduce aerodynamic drag by 25% which would translate to 12% improved fuel economy or 4,200 million gal/year. Objectives are: (1) In support of DOE's mission, provide guidance to industry in the reduction of aerodynamic drag; (2) To shorten and improve design process, establish a database of experimental, computational, and conceptual design information; (3) Demonstrate new drag-reduction techniques; and (4) Get devices on the road. Some accomplishments are: (1) Concepts developed/tested that exceeded 25% drag reduction goal; (2) Insight and guidelines for drag reduction provided to industry through computations and experiments; (3) Joined with industry in getting devices on the road and providing design concepts through virtual modeling and testing; and (4) International recognition achieved through open documentation and database.

  10. Aerodynamic pressure and flow-visualization measurement from a rotating wind turbine blade

    SciTech Connect (OSTI)

    Butterfield, C.P.

    1988-11-01

    Aerodynamic, load, flow-visualization, and inflow measurements have been made on a 10-m, three-bladed, downwind, horizontal-axis wind turbine (HAWT). A video camera mounted on the rotor was used to record nighttime and daytime video images of tufts attached to the low-pressure side of a constant-chord, zero-twist blade. Load measurements were made using strain gages mounted at every 10% of the blade's span. Pressure measurements were made at 80% of the blade's span. Pressure taps were located at 32 chordwise positions, revealing pressure distributions comparable with wind tunnel data. Inflow was measured using a vertical-plane array of eight propvane and five triaxial (U-V-W) prop-type anemometers located 10 m upwind in the predominant wind direction. One objective of this comprehensive research program was to study the effects of blade rotation on aerodynamic behavior below, near, and beyond stall. To this end, flow patterns are presented here that reveal the dynamic and steady behavior of flow conditions on the blade. Pressure distributions are compared to flow patterns and two-dimensional wind tunnel data. Separation boundary locations are shown that change as a function of spanwise location, pitch angle, and wind speed. 6 refs., 23 figs., 1 tab.

  11. Critical behavior of the Widom-Rowlinson mixture: coexistence diameter and order parameter

    E-Print Network [OSTI]

    R. L. C. Vink

    2006-01-04

    The critical behavior of the Widom-Rowlinson mixture [J. Chem. Phys. 52, 1670 (1970)] is studied in d=3 dimensions by means of grand canonical Monte Carlo simulations. The finite size scaling approach of Kim, Fisher, and Luijten [Phys. Rev. Lett. 91, 065701 (2003)] is used to extract the order parameter and the coexistence diameter. It is demonstrated that the critical behavior of the diameter is dominated by a singular term proportional to t^(1-alpha), with t the relative distance from the critical point, and alpha the critical exponent of the specific heat. No sign of a term proportional to t^(2beta) could be detected, with beta the critical exponent of the order parameter, indicating that pressure-mixing in this model is small. The critical density is measured to be rho*sigma^3 = 0.7486 +/- 0.0002, with sigma the particle diameter. The critical exponents alpha and beta, as well as the correlation length exponent nu, are also measured and shown to comply with d=3 Ising criticality.

  12. Laboratory evaluation of fan/filter units' aerodynamic and energy performance

    SciTech Connect (OSTI)

    Xu, Tengfang; Jeng, Ming-Shan

    2004-07-27

    The paper discusses the benefits of having a consistent testing method to characterize aerodynamic and energy performance of FFUs. It presents evaluation methods of laboratory-measured performance of ten relatively new, 1220 mm x 610 mm (or 4 ft x 2 ft) fan-filter units (FFUs), and includes results of a set of relevant metrics such as energy performance indices (EPI) based upon the sample FFUs tested. This paper concludes that there are variations in FFUs' performance, and that using a consistent testing and evaluation method can generate compatible and comparable FFU performance information. The paper also suggests that benefits and opportunities exist for our method of testing FFU energy performance to be integrated in future recommended practices.

  13. Investigation of Tractor Base Bleeding for Heavy Vehicle Aerodynamic Drag Reduction

    SciTech Connect (OSTI)

    Ortega, J; Salari, K; Storms, B

    2007-10-25

    One of the main contributors to the aerodynamic drag of a heavy vehicle is tractor-trailer gap drag, which arises when the vehicle operates within a crosswind. Under this operating condition, freestream flow is entrained into the tractor-trailer gap, imparting a momentum exchange to the vehicle and subsequently increasing the aerodynamic drag. While a number of add-on devices, including side extenders, splitter plates, vortex stabilizers, and gap sealers, have been previously tested to alleviate this source of drag, side extenders remain the primary add-on device of choice for reducing tractor-trailer gap drag. However, side extenders are not without maintenance and operational issues. When a heavy vehicle pivots sharply with respect to the trailer, as can occur during loading or unloading operations, the side extenders can become crushed against the trailer. Consequently, fleet operators are forced to incur additional costs to cover the repair or replacement of the damaged side extenders. This issue can be overcome by either shortening the side extenders or by devising an alternative drag reduction concept that can perform just as effectively as side extenders. To explore such a concept, we investigate tractor base bleeding as a means of reducing gap drag. Wind tunnel measurements are made on a 1:20 scale heavy vehicle model at a vehicle width-based Reynolds number of 420,000. The tractor bleeding flow, which is delivered through a porous material embedded within the tractor base, is introduced into the tractor-trailer gap at bleeding coefficients ranging from 0.0-0.018. To determine the performance of tractor base bleeding under more realistic operating conditions, computational fluid dynamics simulations are performed on a full-scale heavy vehicle within a crosswind for bleeding coefficients ranging from 0.0-0.13.

  14. Computing median and antimedian sets in median graphs Kannan Balakrishnan

    E-Print Network [OSTI]

    Klavzar, Sandi

    , Slovenia bostjan.bresar@uni-mb.si Manoj Changat Department of Futures Studies University of Kerala. Subhamathi Department of Futures Studies University of Kerala, Trivandrum-695034, India ajithars

  15. Computing median and antimedian sets in median graphs # Kannan Balakrishnan

    E-Print Network [OSTI]

    Klavzar, Sandi

    , Slovenia bostjan.bresar@uni­mb.si Manoj Changat Department of Futures Studies University of Kerala.kovse@gmail.com Ajitha R. Subhamathi Department of Futures Studies University of Kerala, Trivandrum­695034, India

  16. UBC Social Ecological Economic Development Studies (SEEDS) Student Report Marketing Strategy for Small Diameter Douglas-fir

    E-Print Network [OSTI]

    UBC Social Ecological Economic Development Studies (SEEDS) Student Report Marketing Strategy the current status of the subject matter of a project/report". #12;Marketing Strategy for Small Diameter Columbia 11 April 2003 #12;ii Executive Summary "Marketing Strategy for Small Diameter Douglas

  17. Allometric estimation of earthworm ash-free dry mass from diameters and lengths of select megascolecid and lumbricid species

    E-Print Network [OSTI]

    Tiegs, Scott

    Allometric estimation of earthworm ash-free dry mass from diameters and lengths of select Enchytraeid a b s t r a c t We present novel length to ash-free dry mass and preclitellar diameter to ash. 1999). Dry mass, or ash-free dry mass (AFDM), provides a measure of biomass that is not influenced

  18. Nanotube diameter optimal for channeling of high-energy particle beam

    E-Print Network [OSTI]

    V. M. Biryukov; S. Bellucci

    2002-06-04

    Channeling of particle beam in straight and bent single-wall nanotubes has been studied in computer simulations. We have found that the nanotubes should be sufficiently narrow in order to steer efficiently the particle beams, with preferred diameter in the order of 0.5-2 nm. Wider nanotubes, e.g. 10-50 nm, appear rather useless for channeling purpose because of high sensitivity of channeling to nanotube curvature. We have compared bent nanotubes with bent crystals as elements of beam steering technique, and found that narrow nanotubes have an efficiency of beam bending similar to that of crystals.

  19. PROCESSING METHOD EFFECT ON SUN DIAMETER MEASUREMENT WITH CCD SOLAR ASTROLABE

    SciTech Connect (OSTI)

    Djafer, Djelloul; Irbah, Abdenour E-mail: abdenour.irbah@latmos.ipsl.fr

    2012-05-01

    Photometric Sun diameter measurement is based on the calculation of the inflection point of the solar limb. In ground measurement, this point is located at a position on the solar limb where the signal-to-noise ratio is very high, which necessitates the appropriate filtering techniques to eliminate the noise while preserving its position. In this paper, we compare the filtering method currently in use to process the CCD solar astrolabe data, the FFTD method widely used, with a different method that we propose. Using the acquired data from the CCD astrolabe at Calern, France during 1997, we can obtain a mean difference of 130 mas in the measured radii.

  20. Using image processing to measure tree crown diameters and estimate percent crown closure

    E-Print Network [OSTI]

    Gabriel, Darren Kyle

    1994-01-01

    Table 3 Table 4 Table 5 Table 6 Table 7 DISCUSSION AND CONCLUSIONS 13 16 18 19 19 20 21 21 23 23 24 24 27 28 30 31 33 35 FUTURE STUDY REFERENCES APPENDIX A APPENDIX B VITA Page 40 80 82 LIST OF TABLES Page TABLE 1 CROWN... DIAMETER RESULTS USING DIFFERENT METHODS OF MEASURE. 25 TABLE 2. DATA USED TO TEST FOR SIGNIFICANCE 26 TABLE 3 DATA USED TO TEST FOR SIGNIFICANCE AND THE Z TEST 27 TABLE 4. TABLE 5. DIFFERENCE BETWEEN CONTROL AND TWO METHODS OF MEASURING CROWN...

  1. Test, Evaluation, and Demonstration of Practical Devices/Systems to Reduce Aerodynamic Drag of Tractor/Semitrailer Combination Unit Trucks

    SciTech Connect (OSTI)

    Scott Smith; Karla Younessi; Matt Markstaller; Dan Schlesinger; Bhaskar Bhatnagar; Donald Smith; Bruno Banceu; Ron Schoon; V.K. Sharma; Mark Kachmarsky; Srikant Ghantae; Michael Sorrels; Conal Deedy; Justin Clark; Skip Yeakel; Michael D. Laughlin; Charlotte Seigler; Sidney Diamond

    2007-04-30

    Class 8 heavy-duty trucks account for over three-quarters of the total diesel fuel used by commercial trucks (trucks with GVWRs more than 10,000 pounds) in the United States each year. At the highway speeds at which these trucks travel (i.e., 60 mph or greater), aerodynamic drag is a major part of total horsepower needed to move the truck down the highway, Reductions in aerodynamic drag can yield measurable benefits in fuel economy through the use of relatively inexpensive and simple devices. The goal of this project was to examine a number of aerodynamic drag reduction devices and systems and determine their effectiveness in reducing aerodynamic drag of Class 8 tractor/semitrailer combination-units, thus contributing to DOE's goal of reducing transportation petroleum use. The project team included major heavy truck manufacturers in the United States, along with the management and industry expertise of the Truck Manufacturers Association as the lead investigative organization. The Truck Manufacturers Association (TMA) is the national trade association representing the major North American manufacturers of Class 6-8 trucks (GVWRs over 19,500 lbs). Four major truck manufacturers participated in this project with TMA: Freightliner LLC; International Truck and Engine Corporation; Mack Trucks Inc.; and Volvo Trucks North America, Inc. Together, these manufacturers represent over three-quarters of total Class 8 truck sales in the United States. These four manufacturers pursued complementary research efforts as part of this project. The project work was separated into two phases conducted over a two-year period. In Phase I, candidate aerodynamic devices and systems were screened to focus research and development attention on devices that offered the most potential. This was accomplished using full-size vehicle tests, scale model tests, and computational fluid dynamics analyses. In Phase II, the most promising devices were installed on full-size trucks and their effect on fuel economy was determined, either through on-road testing or full-size wind tunnel testing. All of the manufacturers worked with devices and systems that offer practical solutions to reduce aerodynamic drag, accounting for functionality, durability, cost effectiveness, reliability, and maintainability. The project team members and their roles and responsibilities are shown in Figure 2-1. Figure 2-2 shows the Phase I and II project schedules for all four projects and associated management activities.

  2. Effects of tone on the three-way laryngeal distinction in Korean: An acoustic and aerodynamic comparison of the Seoul and South Kyungsang dialects

    E-Print Network [OSTI]

    Lee, Hyunjung; Jongman, Allard

    2012-08-01

    The three-way laryngeal distinction among voiceless Korean stops has been well documented for the Seoul dialect. The present study compares the acoustic and aerodynamic properties of this stop series between two dialects, non-tonal Seoul and tonal...

  3. Feasibility of in situ lining rehabilitation of small diameter heat distribution pipe

    SciTech Connect (OSTI)

    Cardenas, H.E.; Hock, V.F.; Segan, E.G. [Army Construction Engineering Research Labs., Champaign, IL (United States)

    1995-12-01

    Many pipeline rehabilitation methods are available for large pipe systems greater than 2 inches in diameter. For small internal systems with many lateral connections, the cost of these methods becomes exorbitant. This study examined the feasibility of an in situ lining rehabilitation concept for small pipelines that involves minimal surface preparation. This work addressed: testing and modification of candidate liner resins, hydraulic analysis of lining impact on pipe flow, and the life cycle cost comparison of applying a liner compared with typical plumbing maintenance practices. Analytical projections based on these analyses revealed a potential source of life cycle cost savings by applying this rehabilitation process to condensate return lines. A liner formulation involving Bisphenol-A and 1% silica addition exhibited sufficient high temperature immersion resistance to operate in a condensate return line. The mathematical liner impact model developed herein provides a qualitative representation of the liner impact on flow. Analytical findings derived from this model indicated that power savings are significantly dependent on pipe diameter and flow rate. A present worth, life cycle cost analysis revealed that if the cost of in situ rehabilitation is roughly 50% of replacement, the benefits may be revealed in terms of avoided operations, maintenance, and repair costs.

  4. THE MEGAMASER COSMOLOGY PROJECT. V. AN ANGULAR-DIAMETER DISTANCE TO NGC 6264 AT 140 Mpc

    SciTech Connect (OSTI)

    Kuo, C. Y.; Braatz, J. A.; Lo, K. Y.; Condon, J. J.; Impellizzeri, C. M. V.; Reid, M. J.; Henkel, C.

    2013-04-20

    We present the direct measurement of the Hubble constant, yielding the direct measurement of the angular-diameter distance to NGC 6264 using the H{sub 2}O megamaser technique. Our measurement is based on sensitive observations of the circumnuclear megamaser disk from four observations with the Very Long Baseline Array, the Green Bank Telescope (GBT), and the Effelsberg telescope. We also monitored the maser spectral profile for 2.3 years using the GBT to measure accelerations of maser lines by tracking their line-of-sight velocities as they change with time. The measured accelerations suggest that the systemic maser spots have a significantly wider radial distribution than in the archetypal megamaser in NGC 4258. We model the maser emission as arising from a circumnuclear disk with orbits dominated by the central black hole. The best fit of the data gives a Hubble constant of H{sub 0} = 68 {+-} 9 km s{sup -1} Mpc{sup -1}, which corresponds to an angular-diameter distance of 144 {+-} 19 Mpc. In addition, the fit also gives a mass of the central black hole of (3.09 {+-} 0.42) Multiplication-Sign 10{sup 7} M{sub Sun }. The result demonstrates the feasibility of measuring distances to galaxies located well into the Hubble flow by using circumnuclear megamaser disks.

  5. MAIN BELT ASTEROIDS WITH WISE/NEOWISE. I. PRELIMINARY ALBEDOS AND DIAMETERS

    SciTech Connect (OSTI)

    Masiero, Joseph R.; Mainzer, A. K.; Bauer, J. M.; Eisenhardt, P. R. M.; DeBaun, E.; Elsbury, D.; Gautier, T. IV; Gomillion, S.; Wilkins, A. [Jet Propulsion Laboratory/California Institute of Technology, Pasadena, CA 91109 (United States); Grav, T. IV [Department of Physics and Astronomy, Johns Hopkins University, Baltimore, MD 21218 (United States); Cutri, R. M.; Dailey, J. [Infrared Processing and Analysis Center, California Institute of Technology, Pasadena, CA 91125 (United States); McMillan, R. S. [Lunar and Planetary Laboratory, University of Arizona, Kuiper Space Science Building 92, Tucson, AZ 85721-0092 (United States); Spahr, T. B. [Minor Planet Center, Harvard-Smithsonian Center for Astrophysics, Cambridge, MA 02138 (United States); Skrutskie, M. F. [Department of Astronomy, University of Virginia, Charlottesville, VA 22903-0818 (United States); Tholen, D. [Institute for Astronomy, University of Hawaii, Honolulu, HI 96822 (United States); Walker, R. G. [Monterey Institute for Research in Astronomy, Monterey, CA (United States); Wright, E. L., E-mail: Joseph.Masiero@jpl.nasa.gov [UCLA Astronomy, Los Angeles, CA 90095-1547 (United States)

    2011-11-10

    We present initial results from the Wide-field Infrared Survey Explorer (WISE), a four-band all-sky thermal infrared survey that produces data well suited for measuring the physical properties of asteroids, and the NEOWISE enhancement to the WISE mission allowing for detailed study of solar system objects. Using a NEATM thermal model fitting routine, we compute diameters for over 100,000 Main Belt asteroids from their IR thermal flux, with errors better than 10%. We then incorporate literature values of visible measurements (in the form of the H absolute magnitude) to determine albedos. Using these data we investigate the albedo and diameter distributions of the Main Belt. As observed previously, we find a change in the average albedo when comparing the inner, middle, and outer portions of the Main Belt. We also confirm that the albedo distribution of each region is strongly bimodal. We observe groupings of objects with similar albedos in regions of the Main Belt associated with dynamical breakup families. Asteroid families typically show a characteristic albedo for all members, but there are notable exceptions to this. This paper is the first look at the Main Belt asteroids in the WISE data, and only represents the preliminary, observed raw size, and albedo distributions for the populations considered. These distributions are subject to survey biases inherent to the NEOWISE data set and cannot yet be interpreted as describing the true populations; the debiased size and albedo distributions will be the subject of the next paper in this series.

  6. Advanced Electric Systems and Aerodynamics for Efficiency Improvements in Heavy Duty Trucks

    SciTech Connect (OSTI)

    Larry Slone; Jeffrey Birkel

    2007-10-31

    The Advanced Electric Systems and Aerodynamics for Efficiency Improvements in Heavy Duty Trucks program (DE-FC26-04NT42189), commonly referred to as the AES program, focused on areas that will primarily benefit fuel economy and improve heat rejection while driving over the road. The AES program objectives were to: (1) Analyze, design, build, and test a cooling system that provided a minimum of 10 percent greater heat rejection in the same frontal area with no increase in parasitic fan load. (2) Realize fuel savings with advanced power management and acceleration assist by utilizing an integrated starter/generator (ISG) and energy storage devices. (3) Quantify the effect of aerodynamic drag due to the frontal shape mandated by the area required for the cooling system. The program effort consisted of modeling and designing components for optimum fuel efficiency, completing fabrication of necessary components, integrating these components into the chassis test bed, completing controls programming, and performance testing the system both on a chassis dynamometer and on the road. Emission control measures for heavy-duty engines have resulted in increased engine heat loads, thus introducing added parasitic engine cooling loads. Truck electrification, in the form of thermal management, offers technological solutions to mitigate or even neutralize the effects of this trend. Thermal control offers opportunities to avoid increases in cooling system frontal area and forestall reduced fuel economy brought about by additional aerodynamic vehicle drag. This project explored such thermal concepts by installing a 2007 engine that is compliant with current regulations and bears additional heat rejection associated with meeting these regulations. This newer engine replaced the 2002 engine from a previous project that generated less heat rejection. Advanced power management, utilizing a continuously optimized and controlled power flow between electric components, can offer additional fuel economy benefits to the heavy-duty trucking industry. Control software for power management brings added value to the power distribution and energy storage architecture on board a truck with electric accessories and an ISG. The research team has built upon a previous truck electrification project, formally, 'Parasitic Energy Loss Reduction and Enabling Technologies for Class 7/8 Trucks', DE-FC04-2000AL6701, where the fundamental concept of electrically-driven accessories replacing belt/gear-driven accessories was demonstrated on a Kenworth T2000 truck chassis. The electrical accessories, shown in Figure 1, were controlled to provide 'flow on demand' variable-speed operation and reduced parasitic engine loads for increased fuel economy. These accessories also provided solutions for main engine idle reduction in long haul trucks. The components and systems of the current project have been integrated into the same Kenworth T2000 truck platform. Reducing parasitic engine loading by decoupling accessory loads from the engine and driving them electrically has been a central concept of this project. Belt or gear-driven engine accessories, such as water pump, air conditioning compressor, or air compressor, are necessarily tied to the engine speed dictated by the current vehicle operating conditions. These conventional accessory pumps are sized to provide adequate flow or pressure at low idle or peak torque speeds, resulting in excess flow or pressure at cruising or rated speeds. The excess flow is diverted through a pressure-minimizing device such as a relief valve thereby expending energy to drive unnecessary and inefficient pump operation. This inefficiency causes an increased parasitic load to the engine, which leads to a loss of usable output power and decreased fuel economy. Controlling variable-speed electric motors to provide only the required flow or pressure of a particular accessory system can yield significant increases in fuel economy for a commercial vehicle. Motor loads at relatively high power levels (1-5 kW, or higher) can be efficiently provided

  7. The Engineering Design of the 1.5 m Diameter Solenoid for the MICERFCC Modules

    SciTech Connect (OSTI)

    Wang, L.; Green, M.A.; Xu, F.Y.; Wu, H.; Li, L.K.; Gou, C.S.; Liu, C.S.; Han, G.; Jia, L.X.; Li, D.; Prestemon, S.O.; Virostek, S.P.

    2007-08-27

    The RF coupling coil (RFCC) module of MICE is where muonsthat have been cooled within the MICE absorber focus (AFC) modules arere-accelerated to their original longitudinal momentum. The RFCC moduleconsists of four 201.25 MHz RF cavities in a 1.4 meter diameter vacuumvessel. The muons are kept within the RF cavities by the magnetic fieldgenerated by a superconducting coupling solenoid that goes around the RFcavities. The coupling solenoid will be cooled using a pair of 4 K pulsetube cooler that will generate 1.5 W of cooling at 4.2 K. The magnet willbe powered using a 300 A two-quadrant power supply. This report describesthe ICST engineering design of the coupling solenoid forMICE.

  8. Demonstration of the BioBaler harvesting system for collection of small-diameter woody biomass

    SciTech Connect (OSTI)

    Langholtz, Matthew H; Caffrey, Kevin R; Barnett, Elliott J; Webb, Erin; Brummette, Mark W; Downing, Mark

    2011-12-01

    As part of a project to investigate sustainable forest management practices for producing wood chips on the Oak Ridge Reservation (ORR) for the ORNL steam plant, the BioBaler was tested in various Oak Ridge locations in August of 2011. The purpose of these tests and the subsequent economic analysis was to determine the potential of this novel woody biomass harvesting method for collection of small-diameter, low value woody biomass. Results suggest that opportunities may exist for economical harvest of low-value and liability or negative-cost biomass. (e.g., invasives). This could provide the ORR and area land managers with a tool to produce feedstock while improving forest health, controlling problem vegetation, and generating local employment.

  9. Design Calculations for Gas Flow & Diffusion Behavior in the large Diameter Container & Cask

    SciTech Connect (OSTI)

    PIEPHO, M.G.

    2003-10-21

    This report describes the calculations for the gas behavior in the void volumes or gas spaces of the sludge Large Diameter Container (LDC) and Cask. The objective is to prevent flammable gas conditions in the LDC and Cask gas spaces. This is achieved by the Active Inert Ventilation System (AIVS), which uses argon gas for dilution purposes. With AIVS, the oxygen content is kept below 5 vol% in the LDC, and the hydrogen content is kept below 4 vol% in the Cask before its purge at the KE Basin. After the Cask sweep-through purge with argon at the KE Basin, oxygen is kept below 5% in both the Cask and the LDC. The analysis here assumes that any oxygen generated in the sludge is consumed by the uranium and uranium dioxide (SNF-18133, ''Gas Behavior in Large Diameter Containers (LDCs) During and Following Loading with 105K East Sludge''). Thus, oxygen production from radiolysis is intentionally not included in this report, but hydrogen from radiolysis and from chemical reactions between uranium and water are considered, depending on the scenario being analyzed. The analysis starts immediately after the final decant at K Basin, when argon is assumed to be the only gas in the LDC gas space, except for the normal water vapor. The oxygen ingress is calculated during the disconnecting of the lines hoses from the LDC, during the time that air is surrounding the LDC with two NucFil-type filters in place after the disconnect, before the Cask is sealed, and, finally, during the sweep-through Cask purge. Dissolution of oxygen from water due to increasing sludge temperatures (mainly during hot transport to the T Plant) is also included.

  10. Inflow Characterization and Aerodynamics Measurements on a SWT-2.3-101 Wind Turbine: Preprint

    SciTech Connect (OSTI)

    Medina, P.; Singh, M.; Johansen, J.; Jove, A.; Fingersh, L.; Schreck, S.

    2012-01-01

    Post processing techniques for aerodynamic data acquired from a Siemens SWT-2.3-101 turbine have been developed and applied in this paper. The turbine is installed at the National Wind Technology Center (NWTC) as part of Cooperative Research And Development Agreement between Siemens Wind Power and the National Renewable Energy Laboratory (NREL) under U.S. Department of Energy (DOE) sponsorship. The results indicate that the use of these corrections is essential for accurate analysis of the data. An example of local inflow angles, velocities, and inflow velocity over the rotor plane derived from measurements from a 5-hole probe is also presented. Finally the pressure measurements are used to characterize unsteady phenomenon, namely, rotational augmentation and dynamic stall on an inboard station. The results show that the rotational augmentation can considerably increase the attached flow regime compared to the 2D CFD results. The dynamic stall event was seen to significantly delay the stall. Furthermore, the nondimensionalized vortex convection derived from the dynamic stall event was found to agree well with results from others studies.

  11. Different methods for particle diameter determination of low density and high density lipoproteins-Comparison and evaluation

    E-Print Network [OSTI]

    Vaidyanathan, Vidya

    2009-05-15

    ) Evaluating the two methods in terms of their ability to identify bi-modal samples. A secondary purpose of this research was to investigate the effect of refrigerated plasma storage on particle diameter. Reproducibility was measured as Coefficient of Variance...

  12. Constructs have shown success in replacement of large-diameter vessels (e.g. thoracic and abdominal aortas,

    E-Print Network [OSTI]

    Sun, Yu

    medium exchange Develop alterna@ve so\\ware environment to simplify Constructs have shown success in replacement of large- diameter vessels (e) constructs have shown more failure rates, resul@ng in aneurysm forma

  13. Effects of Carbon Nanotube Coating on Bubble Departure Diameter and Frequency in Pool Boiling on a Flat, Horizontal Heater

    E-Print Network [OSTI]

    Glenn, Stephen T.

    2011-08-08

    The effects of a carbon nanotube (CNT) coating on bubble departure diameter and frequency in pool boiling experiments was investigated and compared to those on a bare silicon wafer. The pool boiling experiments were performed at liquid subcooling...

  14. Design Calculations for Gas Flow & Diffusion Behavior in the Large Diameter Container & Cask

    SciTech Connect (OSTI)

    PIEPHO, M.G.

    2003-11-06

    This report describes the calculations for the gas behavior in the void volumes or gas spaces of the sludge Large Diameter Container (LDC) and Cask. The objective is to prevent flammable gas conditions in the LDC and Cask gas spaces. This is achieved by the Active Inert Ventilation System (AIVS), which uses argon gas for dilution purposes. With AIVS, the oxygen content is kept below 4 to 5 vol% in the LDC, and the hydrogen content is kept below 4 vol% in the Cask before its purge at the KE Basin. After the Cask sweep-through purge with argon at the KE Basin, oxygen stays below 4 to 5% in the LDC until two LDC ports are opened at T Plant. The oxygen content stays below 4% in the Cask until the Cask lid is opened at T Plant. The analysis here assumes that any oxygen generated in the sludge is consumed by the uranium and uranium dioxide (SNF-18133, ''Gas Behavior in Large Diameter Containers (LDCs) During and Following Loading with 105K East Sludge''). Thus, oxygen production from radiolysis is not included in this report, but hydrogen from radiolysis and from chemical reactions between uranium and water are considered, depending on the scenario being analyzed. The analysis starts immediately after the final decant at K Basin, when argon is assumed to be the only gas in the LDC gas space, except for the normal water vapor. The oxygen ingress is calculated during the disconnecting of the lined hoses from the LDC, during the time that air is surrounding the LDC with two NucFil-type filters in place after the disconnect, before the Cask is sealed, and, finally, during the sweep-through Cask purge at the KE Basin. Dissolution of oxygen from water due to increasing sludge temperatures (mainly during hot transport to the T Plant) is also included. The analysis includes the gas behavior during the T-Plant operations, which include the venting after the LDC/Cask are received at T Plant, the Cask sweep-through purge, the LDC purge with forced argon delivery into the LDC with 1 open port, followed by the natural sweep-through purge with two open LDC ports.

  15. Turbulence loads on the Howden 26-m-diameter wind turbine

    SciTech Connect (OSTI)

    Madsen, P.H.; Hock, S.M.; Hausfeld, T.E.

    1987-11-01

    Conducted in Palm Springs, California, a joint effort between SERI and James Howden and Company involved a comprehensive test program on the 330-kW Howden wind turbine with a three-bladed, fixed-hub rotor 26 m in diameter. Part of the measurement analysis is to quantify the turbulence loads during the steady-state production modes of operation. Assuming wind turbulence to be the cause of the random loads, the turbulence loads in terms of blade root-bending moments have been determined empirically by isolating the random or nonperiodic part of the load signals using azimuthal averaging. Standard deviations as functions of wind speed, as well as power spectra of the loads, are presented. The measured turbulence loads are compared to a recently developed model for turbulence loading of wind turbines. The model works in the frequency domain and uses the standard engineering representation of turbulence in terms of a coherence function and a wind-power spectrum at a fixed point in space. The turbulence load model accounts for the dominant mode of vibration for the load in question and is intended to be simple enough to be used for a preliminary load estimate for practical design purposes.

  16. Apparatus and method for increasing the diameter of metal alloy wires within a molten metal pool

    DOE Patents [OSTI]

    Hartman, Alan D. (Albany, OR); Argetsinger, Edward R. (Albany, OR); Hansen, Jeffrey S. (Corvallis, OR); Paige, Jack I. (Albany, OR); King, Paul E. (Corvallis, OR); Turner, Paul C. (Independence, OR)

    2002-01-29

    In a dip forming process the core material to be coated is introduced directly into a source block of coating material eliminating the need for a bushing entrance component. The process containment vessel or crucible is heated so that only a portion of the coating material becomes molten, leaving a solid portion of material as the entrance port of, and seal around, the core material. The crucible can contain molten and solid metals and is especially useful when coating core material with reactive metals. The source block of coating material has been machined to include a close tolerance hole of a size and shape to closely fit the core material. The core material moves first through the solid portion of the source block of coating material where the close tolerance hole has been machined, then through a solid/molten interface, and finally through the molten phase where the diameter of the core material is increased. The crucible may or may not require water-cooling depending upon the type of material used in crucible construction. The system may operate under vacuum, partial vacuum, atmospheric pressure, or positive pressure depending upon the type of source material being used.

  17. Are non-magnetic mechanisms such as temporal solar diameter variations conceivable for an irradiance variability?

    E-Print Network [OSTI]

    J. P. Rozelot; S. Lefebvre; S. Pireaux; A. Ajabshirizadeh

    2006-01-05

    Irradiance variability has been monitored from space for more than two decades. Even if data are coming from different sources, it is well established that a temporal variability exists which can be set to as approximately 0.1%, in phase with the solar cycle. Today, one of the best explanation for such an irradiance variability is provided by the evolution of the solar surface magnetic fields. But if some 90 to 95% can be reproduced, what would be the origin of the 10 to 5% left? Non magnetic effects are conceivable. In this paper we will consider temporal variations of the diameter of the Sun as a possible contributor for the remaining part. Such an approach imposes strong constraints on the solar radius variability. We will show that over a solar cycle, variations of no more than 20 mas of amplitude can be considered. Such a variability (far from what is reported by observers conducting measurements by means of ground-based solar astrolabes) may explain a little part of the irradiance changes not explained by magnetic features. Further requirements are needed that may help to reach a conclusion. Dedicated space missions are necessary (for example PICARD, GOLF-NG or SDO, scheduled for a launch around 2008); it is also proposed to reactivate SDS flights for such a purpose.

  18. Large-diameter coiled tubing completions decrease risk of formation damage

    SciTech Connect (OSTI)

    Norton, V. ); Edens, F. ); Coker, G. ); King, G. )

    1992-07-20

    Amoco Production Co. has used large-diameter coiled tubing strings to avoid damaging gas wells with kill fluids. The coiled tubing is stripped in the gas well under pressure. In Amoco's case, the gas flows up the tubing/casing annulus. The coiled tubing string provides a way to blow down the well whenever the well loads up with liquids from completion, workover, or naturally produced fluids. This paper reports that to date, Amoco has installed coiled tubing in four wells. The oldest has 18 months of service. Although some turbine longevity questions must be answered, the first four completions have proven fast and trouble free. The basic equipment for handling coil tubing is shown. The transport trailer and tubing injector head are similar to standard servicing equipment and not considered experimental. The production tubing reel is capable of carrying 14,000 ft of 2-in tubing or 18,000 ft of 1 3/4-in. tubing. For shallower wells, multiple tubing strings can be would on the same spool. Because of handling difficulties of large tubing, spools must be wound at the factory. Most of the largest sizes are made to order, making lead time a necessary consideration.

  19. Method and apparatus for controlling current in inductive loads such as large diameter coils

    DOE Patents [OSTI]

    Riveros, Carlos A. (3832 Harrison Ave., Brookfield, IL 60513)

    1981-01-01

    A method and apparatus for controlling electric current in loads that are essentially inductive, such that sparking and "ringing" current problems are reduced or eliminated. The circuit apparatus employs a pair of solid state switches (each of which switch may be an array of connected or parallel solid state switching devices such as transistors) and means for controlling those switches such that a power supply supplying two d.c. voltages (e.g. positive 150 volts d.c. and negative 150 volts d.c.) at low resistance may be connected across an essentially inductive load (e.g. a 6 gauge wire loop one hundred meters in diameter) alternatively and such that the first solid state switch is turned off and the second is turned on such that both are not on at the same time but the first turned on and the other on in less time than the inductive time constant (L/R) so that the load is essentially always presented with a low resistance path across its input. In this manner a steady AC current may be delivered to the load at a frequency desired. Shut-off problems are avoided by gradually shortening the period of switching to less than the time constant so that the maximum energy contained in the inductive load is reduced to approximately zero and dissipated in the inherent resistance. The invention circuit may be employed by adjusting the timing of switching to deliver a desired waveform (such as sinusoidal) to the load.

  20. Apparatus and Method for Increasing the Diameter of Metal Alloy Wires Within a Molten Metal Pool

    DOE Patents [OSTI]

    Hartman, Alan D.; Argetsinger, Edward R.; Hansen, Jeffrey S.; Paige, Jack I.; King, Paul E.; Turner, Paul C.

    2002-01-29

    In a dip forming process the core material to be coated is introduced directly into a source block of coating material eliminating the need for a bushing entrance component. The process containment vessel or crucible is heated so that only a portion of the coating material becomes molten, leaving a solid portion of material as the entrance port of, and seal around, the core material. The crucible can contain molten and solid metals and is especially useful when coating core material with reactive metals. The source block of coating material has been machined to include a close tolerance hole of a size and shape to closely fit the core material. The core material moves first through the solid portion of the source block of coating material where the close tolerance hole has been machined, then through a solid/molten interface, and finally through the molten phase where the diameter of the core material is increased. The crucible may or may not require water-cooling depending upon the type of material used in crucible construction. The system may operate under vacuum, partial vacuum, atmospheric pressure, or positive pressure depending upon the type of source material being used.

  1. September 2002 Working Group Meeting on Heavy Vehicle Aerodynamic Drag: Presentations and Summary of Comments and Conclusions

    SciTech Connect (OSTI)

    McCallen, R

    2002-09-01

    A Working Group Meeting on Heavy Vehicle Aerodynamic Drag was held at NASA Ames Research Center on September 23, 2002. The purpose of the meeting was to present and discuss technical details on the experimental and computational work in progress and future project plans. Representatives from the Department of Energy (DOE)/Office of Energy Efficiency and Renewable Energy/Office of FreedomCAR & Vehicle Technologies, Lawrence Livermore National Laboratory (LLNL), Sandia National Laboratories (SNL), NASA Ames Research Center (NASA), University of Southern California (USC), California Institute of Technology (Caltech), Georgia Tech Research Institute (GTRI), Argonne National Laboratory (ANL), Freightliner, and Portland State University participated in the meeting. This report contains the technical presentations (viewgraphs) delivered at the Meeting, briefly summarizes the comments and conclusions, and outlines the future action items. The meeting began with an introduction by the Project Lead Rose McCallen of LLNL, where she emphasized that the world energy consumption is predicted to relatively soon exceed the available resources (i.e., fossil, hydro, non-breeder fission). This short fall is predicted to begin around the year 2050. Minimizing vehicle aerodynamic drag will significantly reduce our Nation's dependence on foreign oil resources and help with our world-wide fuel shortage. Rose also mentioned that educating the populace and researchers as to our world energy issues is important and that our upcoming United Engineering Foundation (UEF) Conference on ''The Aerodynamics of Heavy Vehicles: Trucks, Busses, and Trains'' was one way our DOE Consortium was doing this. Mentioned were the efforts of Fred Browand from USC in organizing and attracting internationally recognized speakers to the Conference. Rose followed with an overview of the DOE project goals, deliverables, and FY03 activities. The viewgraphs are attached at the end of this report. Sid Diamond of DOE discussed the reorganization of the Office of Energy Efficiency and Renewable Energy and that the Office of Heavy Vehicle Technology is now part of the Office of FreedomCAR & Vehicle Technologies. Sid reviewed the FY03 budget and provided information on some plans for FY04. The soon to be posted DOE request for proposals from industry for projects related to parasitic energy losses was discussed. A minimum of 50% cost share by industry will be required and the proposal must be submitted by industry. Collaborative efforts in aerodynamic drag with members of the DOE consortium are encouraged. Sid also mentioned interest in aerodynamic drag contribution due to wheel wells and underbody flow. Sid also mentioned his continued interest in the application of our computational and experimental expertise to the area of locomotive and railcar aerodynamics for the reduction of drag effects and thus, the reduction of fuel consumption by trains. In summary, the technical presentations at the meeting included a review of experimental results and plans by GTRI, USC, and NASA Ames, the computational results from LLNL and SNL for the integrated tractor-trailer benchmark geometry called the Ground Transportation System (GTS) model, and by LLNL for the tractor-trailer gap and trailer wake flow, and turbulence model development and benchmark simulations being investigated by Caltech. USC is also investigating an acoustic drag reduction device that has been named ''Mozart'', GTRI continues their investigation of a blowing device, and LLNL presented their ideas for 2 new base drag reduction devices. ANL presented their plans for a DOE supported Cooperative Research and Development Agreement (CRADA) with Paccar Truck Company utilizing commercial software tools to simulate the flow and drag for an actual tractor and showed the results of some preliminary griding attempts. The attendees also had the opportunity to tour the 12-ft pressure wind tunnel the machine shop were the Generic Conventional Model (GCM, a.k.a. SLRT) was being readied for the scheduled November experiments. Much of

  2. Plasma sputtering robotic device for in-situ thick coatings of long, small diameter vacuum tubes

    SciTech Connect (OSTI)

    Hershcovitch, A. Blaskiewicz, M.; Brennan, J. M.; Fischer, W.; Liaw, C.-J.; Meng, W.; Todd, R.; Custer, A.; Dingus, A.; Erickson, M.; Jamshidi, N.; Laping, R.; Poole, H. J.

    2015-05-15

    A novel robotic plasma magnetron mole with a 50?cm long cathode was designed, fabricated, and operated. The reason for this endeavor is to alleviate the problems of unacceptable resistive heating of stainless steel vacuum tubes in the BNL Relativistic Heavy Ion Collider (RHIC). The magnetron mole was successfully operated to copper coat an assembly containing a full-size, stainless steel, cold bore, RHIC magnet tubing connected to two types of RHIC bellows, to which two additional pipes made of RHIC tubing were connected. To increase the cathode lifetime, a movable magnet package was developed, and the thickest possible cathode was made, with a rather challenging target to substrate (de facto anode) distance of less than 1.5?cm. Achieving reliable steady state magnetron discharges at such a short cathode to anode gap was rather challenging, when compared to commercial coating equipment, where the target to substrate distance is 10's cm; 6.3?cm is the lowest experimental target to substrate distance found in the literature. Additionally, the magnetron developed during this project provides unique omni-directional uniform coating. The magnetron is mounted on a carriage with spring loaded wheels that successfully crossed bellows and adjusted for variations in vacuum tube diameter, while keeping the magnetron centered. Electrical power and cooling water were fed through a cable bundle. The umbilical cabling system is driven by a motorized spool. Excellent coating adhesion was achieved. Measurements indicated that well-scrubbed copper coating reduced secondary electron yield to 1, i.e., the problem of electron clouds can be eliminated. Room temperature RF resistivity measurement indicated that a 10??m copper coated stainless steel RHIC tube has a conductivity close to that of pure copper tubing. Excellent coating adhesion was achieved. The device details and experimental results are described.

  3. Transits of Venus and Solar diameter measures from ground: method and results from Athens (2004) and Huairou (2012)

    E-Print Network [OSTI]

    Sigismondi, Costantino; Wang, Xiaofan; Xie, Wenbin; Carinci, Massimo; Mimmo, Alessio

    2015-01-01

    The variation of the solar diameter in time and in position angle has implications in astrophysics and in general relativity, as the long series of studies attest. The Transits of Venus in 2004 and 2012 have been carefully studied because of the rarity of the phenomenon and its historical importance due the AU measure and to the discovery of Venus atmosphere. The characterization of Venus atmosphere and the measure of the solar diameter to the milliarcsecond level of precision have been studied also from satellite images. The results of the solar diameter measurements made with the observations in Athens (2004) and at the Huairou Solar Observing Station in China (2012) are presented. The topic of the oblateness of the Sun at sunset and its intrinsic value is drafted to introduce the general public to the relativistic relevance of measuring the solar figure, in the occasion of the International Year of Light 2015.

  4. Variation of xylem vessel diameters in trembling aspen (Populus tremuloides Michx.) across a boreal climate gradient: answers from a reciprocal transplant experiment

    E-Print Network [OSTI]

    Hamann, Andreas

    . Gaussian kernel density estimates support plastic as well as genetic contributions in vessel diameter with vessel diameter and tree height in central Alberta was also found at two other boreal test sites but reversed at a wetter and milder sub-boreal test site. 5. In summary, vessel diameters were highly plastic

  5. This is a preprint of the following article, which is available from http://mdolab.engin.umich.edu Zhoujie Lyu and J. R. R. A. Martins. Aerodynamic Shape Optimization Investigations of the Common

    E-Print Network [OSTI]

    Papalambros, Panos

    , and the geometries and meshes for both the baseline and optimized wings are available as supplemental materials://mdolab.engin.umich.edu Zhoujie Lyu and J. R. R. A. Martins. Aerodynamic Shape Optimization Investigations of the Common Research this preprint. Aerodynamic Shape Optimization Investigations of the Common Research Model Wing Benchmark Zhoujie

  6. A survey of ideal fluid propeller theories and a study of the effects of aerodynamic propeller loading on trailing vortex induced velocity and thrust

    E-Print Network [OSTI]

    Kelley, Edward Madison

    1969-01-01

    A SURVEY OF IDEAL FLUID PRO~ THEORIES AND A STUIE OP THE EFFECTS OF AERODYNAMIC PRO~ LOADING ON TRAILING VORTEX INDUCED VELOCITY AND THRUST A Thesis EDWARD MADISON ~ Suhmitted to the Graduate College of Texas A&M University in Partial... VELOCITY AND THRUST A Thesis by EDWARD MADISON HELLEY Approsed as to sty1e and content 'by: Head of epartment i%. mbe August 1969 111 ABSTRACT A Survey of Ideal Fluid Propeller Theories and a Study of the Ei'fects of Aerodynamic Propeller...

  7. UBC Social Ecological Economic Development Studies (SEEDS) Student Report Marketing Strategies for Commercializing the Small Diameter Douglas-fir

    E-Print Network [OSTI]

    UBC Social Ecological Economic Development Studies (SEEDS) Student Report Marketing Strategies the current status of the subject matter of a project/report". #12;WOOD 465 ASSIGNMENT Marketing Strategies may think of this huge market and find a new way to commercialize our small diameter Douglas

  8. Salt-Dependent DNA Superhelix Diameter Studied by Small Angle Neutron Scattering Measurements and Monte Carlo Simulations

    E-Print Network [OSTI]

    Langowski, Jrg

    Salt-Dependent DNA Superhelix Diameter Studied by Small Angle Neutron Scattering Measurements-38042 Grenoble Cedex 9, France ABSTRACT Using small angle neutron scattering we have measured the static the same behavior between 10 and 100 mM salt concentration: An undulation in the scattering curve

  9. Effects of the hydraulic coupling between xylem and phloem on diurnal phloem diameter variationpce_2275 690..703

    E-Print Network [OSTI]

    Holbrook, N. Michele

    Effects of the hydraulic coupling between xylem and phloem on diurnal phloem diameter variationpce in the radial flow rate of water between the xylem and the phloem. Reducing the hydraulic con- ductance between variations that cannot be explained by changes in the hydraulic conductance, could be related to changes

  10. Constructing a Balanced, (log(N)/loglog(N))-Diameter Super-Peer Topology for Scalable P2P Systems

    E-Print Network [OSTI]

    Reeves, Douglas S.

    Constructing a Balanced, (log(N)/loglog(N))-Diameter Super-Peer Topology for Scalable P2P Systems Young June Pyun Department of Computer Science North Carolina State University Raleigh, North Carolina yjpyun@unity.ncsu.edu Douglas S. Reeves Departments of Computer Science and Electrical and Computer

  11. Spray coating as a simple method to prepare catalyst for growth of diameter-tunable single-walled carbon nanotubes

    E-Print Network [OSTI]

    Maruyama, Shigeo

    Spray coating as a simple method to prepare catalyst for growth of diameter-tunable single in simplicity and scalability -- have been recently reported. Dip-coating,[7] drop-casting,[8] and spin-coating quality SWCNTs from catalyst prepared by a spray coating technique, which had previously only been able

  12. A study on the characteristics of upward air-water two-phase flow in a large diameter pipe

    SciTech Connect (OSTI)

    Shen, Xiuzhong; Saito, Yasushi; Mishima, Kaichiro [Research Reactor Institute, Kyoto University, Kumatori-cho, Sennan-gun, Osaka 590-0494 (Japan); Nakamura, Hideo [Nuclear Safety Research Center, Japan Atomic Energy Agency, Tokai-mura, Ibaraki 319-1195 (Japan)

    2006-10-15

    An adiabatic upward co-current air-water two-phase flow in a vertical large diameter pipe (inner diameter, D: 0.2m, ratio of pipe length to diameter, L/D: 60.5) was experimentally investigated under various inlet conditions. Flow regimes were visually observed, carefully analyzed and classified into five, i.e. undisturbed bubbly, agitated bubbly, churn bubbly, churn slug and churn froth. Void fraction, bubble frequency, Sauter mean diameter, interfacial area concentration (IAC) and interfacial direction were measured with four-sensor optical probes. Both the measured void fraction and the measured IAC demonstrated radial core-peak distributions in most of the flow regimes and radial wall peak in the undisturbed bubbly flow only. The bubble frequency also showed a wall-peak radial distribution only when the bubbles were small in diameter and the flow was in the undisturbed bubbly flow. The Sauter mean diameter of bubbles did not change much in the radial direction in undisturbed bubbly, agitated bubbly and churn bubbly flows and showed a core-peak radial distribution in the churn slug flow due to the existence of certain amount of large and deformed bubbles in this flow regime. The measurements of interfacial direction showed that the main and the secondary bubbly flow could be displayed by the main flow peak and the secondary flow peak, respectively, in the probability density function (PDF) of the interfacial directional angle between the interfacial direction and the z-axis, {eta}{sub zi}. The local average {eta}{sub zi }at the bubble front or rear hemisphere ({eta}{sub zi}{sup F} and {eta}{sub zi}{sup R}) reflected the local bubble movement and was in direct connection with the flow regimes. Based on the analysis, the authors classified the flow regimes in the vertical large diameter pipe quantitatively by the cross-sectional area-averaged {eta}{sub zi }at bubbly front hemisphere ({eta}{sub zi}{sup F}-bar). Bubbles in the undisturbed bubbly flow moved in a vertical way with some swerving motions and those in other flow regimes moved along the lateral secondary flow with an averaging net upward velocity. (author)

  13. 21st AIAA Computational Fluid Dynamics Conference, June 24-27, 2013, San Diego, CA Toward High-Fidelity Aerodynamic Shape

    E-Print Network [OSTI]

    Zingg, David W.

    High-Fidelity Aerodynamic Shape Optimization for Natural Laminar Flow Ramy Rashad and David W. Zingg-constrained drag minimization of airfoils at various flight conditions, leading to natural laminar flow designs. I the feasibility of natural laminar flow (NLF) as a key enabler of environmentally responsible commercial aviation

  14. Journal of Wind Engineering and Industrial Aerodynamics, 36 (1990) 1-15 1 ElsevierSciencePublishersB.V.,Amsterdam--Printed in The Netherlands

    E-Print Network [OSTI]

    Kareem, Ahsan

    1990-01-01

    and transport, heat transport and transfer, and sound and light transmission are discussed, and a list the following topics: 1. 2. 3. 4. 5. 6. 7. 8. 9. 10. 11. 12. 13. Theme Lectures BluffBody Aerodynamics Analysis Modelling and System Identification Tall Buildings Structural Glazing and Curtain Walls Mitigation

  15. Wind Tunnel Aerodynamic Tests of Six Airfoils for Use on Small Wind Turbines; Period of Performance: October 31, 2002--January 31, 2003

    SciTech Connect (OSTI)

    Selig, M. S.; McGranahan, B. D.

    2004-10-01

    Wind Tunnel Aerodynamic Tests of Six Airfoils for Use on Small Wind Turbinesrepresents the fourth installment in a series of volumes documenting the ongoing work of th University of Illinois at Urbana-Champaign Low-Speed Airfoil Tests Program. This particular volume deals with airfoils that are candidates for use on small wind turbines, which operate at low Reynolds numbers.

  16. 31st AIAA Applied Aerodynamics Conference, June 24-27, 2013, San Diego, CA Results from the Fifth AIAA Drag Prediction

    E-Print Network [OSTI]

    Zingg, David W.

    is shown to have a significant impact on the recirculation patterns observed at higher angles of attack as an invaluable tool in comparing the accuracy of the solver against established algorithms such as CFL3D4 and FUN in Computational Aerodynamics and Environmentally-Friendly Aircraft Design, J. Armand Bombardier Foundation Chair

  17. The effect of voltage waveform and tube diameter on transporting cold plasma strings through a flexible dielectric tube

    SciTech Connect (OSTI)

    Sohbatzadeh, Farshad; Omran, Azadeh Valinataj

    2014-11-15

    In this work, we developed transporting atmospheric pressure cold plasma using single electrode configuration through a sub-millimetre flexible dielectric tube beyond 100?cm. It was shown that the waveform of the applied high voltage is essential for controlling upstream and downstream plasma inside the tube. In this regard, sawtooth waveform enabled the transport of plasma with less applied high voltage compared to sinusoidal and pulsed form voltages. A cold plasma string as long as 130?cm was obtained by only 4?kV peak-to-peak sawtooth high voltage waveform. Optical emission spectroscopy revealed that reactive chemical species, such as atomic oxygen and hydroxyl, are generated at the tube exit. The effect of tube diameter on the transported plasma was also examined: the smaller the diameter, the higher the applied voltage. The device is likely to be used for sterilization, decontamination, and therapeutic endoscopy as already suggested by other groups in recent past years.

  18. The application of the fusion method of thermit welding to small diameter tubing: An analysis of joint geometry.

    E-Print Network [OSTI]

    Glynn, Thomas Michael

    1972-01-01

    THE APPLICATION OF THE FUSION METHOD OF THERPIIT LIELOING TO SMALL DIAMETER TUBING: AN ANALYSIS OF DOINT GEOMETRY A Thesis by THOMAS MICHAEL GLYNN Submitted to the Graduate College of Texas 48PI University in partial fulfillment... of the requirement for the degree of PIASTER OF SCIENCE December 1972 Major Subject: Industrial Technology THE APPLICATION OF THE FUSION METHOD OF THERMIT 4IELDING TO SMALL DIAPIETER TUBING: AN ANALYSIS OF ANOINT GEOMETRY A Thesis by THOMAS PIICHAEL GLYNN...

  19. Steam-water two-phase flow in large diameter vertical piping at high pressures and temperatures

    SciTech Connect (OSTI)

    Hasanein, H.A.; Kawaji, Masahiro [Univ. of Toronto, Ontario (Canada); Chan, A.M.C. [Ontario Hydro Technologies, Toronto, Ontario (Canada); Yoshioka, Yuzuru [Japan Atomic Power Co., Tokyo (Japan)

    1996-08-01

    No information on steam/water two-phase flow behavior in large diameter pipes (10 inch or larger) at elevated pressures is available in the open literature. However, there are many applications, in the nuclear, chemical and petroleum industries among others where two-phase flows in large diameter pipes at elevated pressures and temperatures are encountered routinely or under accident scenarios. Experimental data on steam-water two-phase flow in a large diameter (20 inch, 50.08 cm I.D.) vertical pipe at elevated pressures and temperatures (2.8 MPa/230 C--6.4 MPa/280 C) have been obtained. Void fraction, two-phase mass flux, phase and velocity distributions as well as pressure drop along the test pipe have been measured using the Ontario Hydro Technologies (OHT) Pump Test Loop. The void fraction distributions were found to be axially symmetric and nearly flat over a wide range of two-phase flow conditions. The two-phase flow regime could be inferred from the dynamic void fluctuations data. For the 280 C tests, the flow was found to be relatively stable with bubbly flow at low average void fractions and churn turbulent or wispy-annular flow at higher void fractions. At 230 C, the flow became rather oscillatory and slugging was suspected at relatively low voids. It has also been found that the average void fractions in the test section can be determined reasonably accurately using the axial pressure drop data.

  20. Session B--Small-Diameter Timber Alchemy--Fried, Barbour, Fight, Christensen, Pinjuv USDA Forest Service Gen. Tech. Rep. PSW-GTR-189. 2008. 29

    E-Print Network [OSTI]

    Session B--Small-Diameter Timber Alchemy--Fried, Barbour, Fight, Christensen, Pinjuv USDA Forest Toward Fire-Resistant Forests?1 Jeremy S. Fried, R. Jamie Barbour, Roger D. Fight, Glenn Christensen- mail: Jeremy.Fried@fs.fed.us. #12;Session B--Small-Diameter Timber Alchemy--Fried, Barbour, Fight

  1. Influence of lubricant oil on heat transfer performance of refrigerant flow boiling inside small diameter tubes. Part I: Experimental study

    SciTech Connect (OSTI)

    Wei, Wenjian; Ding, Guoliang; Hu, Haitao; Wang, Kaijian

    2007-10-15

    Two-phase flow pattern and heat transfer characteristics of refrigerant-oil mixture flow boiling inside small tubes with inside diameters of 6.34 mm and 2.50 mm are investigated experimentally. The test condition of nominal oil concentration is from 0% to 5%, mass flux from 200 to 400 kg m{sup -2} s{sup -1}, heat flux from 3.2 to 14 kW m{sup -2}, evaporation temperature of 5 C, inlet quality from 0.1 to 0.8, and quality change from 0.1 to 0.2. Wavy, wavy-annular, annular and mist-annular flow pattern in 6.34 mm tube are observed, while only slug-annular and annular flow pattern are observed in 2.50 mm tube. Oil presence can make annular flow to form early and to retard to diminish in quality direction at nominal oil concentration {>=}3%. Augmentation effect of oil on heat transfer coefficient becomes weakened or even diminishes for small diameter tube while detrimental effect of oil on small tube performance becomes more significant than large tube. For both test tubes, variation of heat transfer coefficient and enhanced factor with oil concentration is irregular. Two-phase heat transfer multiplier with refrigerant-oil mixture properties increases consistently and monotonically with local oil concentration at different vapor quality. (author)

  2. Ionic transport through sub-10 nm diameter hydrophobic high-aspect ratio nanopores: experiment, theory and simulation

    E-Print Network [OSTI]

    Sbastien Balme; Fabien Picaud; Manoel Manghi; John Palmeri; Mikhael Bechelany; Simon Cabello-Aguilar; Adib Abou-Chaaya; Philippe Miele; Emmanuel Balanzat; Jean Marc Janot

    2015-06-11

    Fundamental understanding of ionic transport at the nanoscale is essential for developing biosensors based on nanopore technology and new generation high-performance nanofiltration membranes for separation and purification applications. We study here ionic transport through single putatively neutral hydrophobic nanopores with high aspect ratio (of length L=6 \\mu m with diameters ranging from 1 to 10 nm) and with a well controlled cylindrical geometry. We develop a detailed hybrid mesoscopic theoretical approach for the electrolyte conductivity inside nanopores, which considers explicitly ion advection by electro-osmotic flow and possible flow slip at the pore surface. By fitting the experimental conductance data we show that for nanopore diameters greater than 4 nm a constant weak surface charge density of about 10$^{-2}$ C m$^{-2}$ needs to be incorporated in the model to account for conductance plateaus of a few pico-Siemens at low salt concentrations. For tighter nanopores, our analysis leads to a higher surface charge density, which can be attributed to a modification of ion solvation structure close to the pore surface, as observed in the molecular dynamics simulations we performed.

  3. Orbital inside diameter welder

    DOE Patents [OSTI]

    Patterson, R.A.; Mitchell, J.O.

    1982-07-23

    The disclosure relates to welding apparatus and more particularly to apparatus for welding together two abutted cylinders from the inside of the joint.

  4. Boattail Plates With Non-Rectangular Geometries For Reducing Aerodynamic Base Drag Of A Bluff Body In Ground Effect

    DOE Patents [OSTI]

    Ortega, Jason M. (Pacifica, CA); Sabari, Kambiz (Livermore, CA)

    2006-03-07

    An apparatus for reducing the aerodynamic base drag of a bluff body having a leading end, a trailing end, a top surface, opposing left and right side surfaces, and a base surface at the trailing end substantially normal to a longitudinal centerline of the bluff body, with the base surface joined (1) to the left side surface at a left trailing edge, (2) to the right side surface at a right trailing edge, and (3) to the top surface at a top trailing edge. The apparatus includes left and right vertical boattail plates which are orthogonally attached to the base surface of the bluff body and inwardly offset from the left and right trailing edges, respectively. This produces left and right vertical channels which generate, in a flowstream substantially parallel to the longitudinal centerline, respective left and right vertically-aligned vortical structures, with the left and right vertical boattail plates each having a plate width defined by a rear edge of the plate spaced from the base surface. Each plate also has a peak plate width at a location between top and bottom ends of the plate corresponding to a peak vortex of the respective vertically-aligned vortical structures.

  5. Influence of lubricant oil on heat transfer performance of refrigerant flow boiling inside small diameter tubes. Part II: Correlations

    SciTech Connect (OSTI)

    Wei, Wenjian; Ding, Guoliang; Hu, Haitao; Wang, Kaijian

    2007-10-15

    The predictive ability of the available state-of-the-art heat transfer correlations of refrigerant-oil mixture is evaluated with the present experiment data of small tubes with inside diameter of 6.34 mm and 2.50 mm. Most of these correlations can be used to predict the heat transfer coefficient of 6.34 mm tube, but none of them can predict heat transfer coefficient of 2.50 mm tube satisfactorily. A new correlation of two-phase heat transfer multiplier with local properties of refrigerant-oil mixture is developed. This correlation approaches the actual physical mechanism of flow boiling heat transfer of refrigerant-oil mixture and can reflect the actual co-existing conditions of refrigerant and lubricant oil. More than 90% of the experiment data of both test tubes have less than {+-}20% deviation from the prediction values of the new correlations. (author)

  6. To obtain representative temperatures, sensors were made with a length of 35 cm. The stainless steel needles have a diameter of 3 mm. Inside are five

    E-Print Network [OSTI]

    Haak, Hein

    To obtain representative temperatures, sensors were made with a length of 35 cm. The stainless steel needles have a diameter of 3 mm. Inside are five Platinum Pt-100 sensors, that are cascaded

  7. The application of the fusion method of thermit welding to small diameter tubing: An analysis of mold design and powder quantity.

    E-Print Network [OSTI]

    Eller, Frank Charles

    1972-01-01

    THE APPLICATION OF THE FUSION METHOD OF THERMIT LIELDING TO SMALL DIAMETER TUBING: AN ANALYSIS OF IYIOLD DESIGN AND POLIDER QUANTITY A Thesis 'by FRANK CHARLES ELLER, OR. Submitted to the Graduate College of Texas AEM University in partial... A Thesis by FRANK CHARLES ELLER, OR. Approved as to style and content by: Chairman of Committee Head of Departm t Member December 1972 A f 111 ABSTRACT The Application of the Fusion Method of Thermit Llelding to Small Diameter Tubing...

  8. Computational mechanics research and support for aerodynamics and hydraulics at TFHRC year 1 quarter 4 progress report.

    SciTech Connect (OSTI)

    Lottes, S.A.; Kulak, R.F.; Bojanowski, C. (Energy Systems)

    2011-12-09

    The computational fluid dynamics (CFD) and computational structural mechanics (CSM) focus areas at Argonne's Transportation Research and Analysis Computing Center (TRACC) initiated a project to support and compliment the experimental programs at the Turner-Fairbank Highway Research Center (TFHRC) with high performance computing based analysis capabilities in August 2010. The project was established with a new interagency agreement between the Department of Energy and the Department of Transportation to provide collaborative research, development, and benchmarking of advanced three-dimensional computational mechanics analysis methods to the aerodynamics and hydraulics laboratories at TFHRC for a period of five years, beginning in October 2010. The analysis methods employ well-benchmarked and supported commercial computational mechanics software. Computational mechanics encompasses the areas of Computational Fluid Dynamics (CFD), Computational Wind Engineering (CWE), Computational Structural Mechanics (CSM), and Computational Multiphysics Mechanics (CMM) applied in Fluid-Structure Interaction (FSI) problems. The major areas of focus of the project are wind and water effects on bridges - superstructure, deck, cables, and substructure (including soil), primarily during storms and flood events - and the risks that these loads pose to structural failure. For flood events at bridges, another major focus of the work is assessment of the risk to bridges caused by scour of stream and riverbed material away from the foundations of a bridge. Other areas of current research include modeling of flow through culverts to assess them for fish passage, modeling of the salt spray transport into bridge girders to address suitability of using weathering steel in bridges, CFD analysis of the operation of the wind tunnel in the TFCHR wind engineering laboratory, vehicle stability under high wind loading, and the use of electromagnetic shock absorbers to improve vehicle stability under high wind conditions. This quarterly report documents technical progress on the project tasks for the period of July through September 2011.

  9. Computational mechanics research and support for aerodynamics and hydraulics at TFHRC, year 2 quarter 2 progress report

    SciTech Connect (OSTI)

    Lottes, S.A.; Bojanowski, C.; Shen, J.; Xie, Z.; Zhai, Y. (Energy Systems); (Turner-Fairbank Highway Research Center)

    2012-06-28

    The computational fluid dynamics (CFD) and computational structural mechanics (CSM) focus areas at Argonne's Transportation Research and Analysis Computing Center (TRACC) initiated a project to support and compliment the experimental programs at the Turner-Fairbank Highway Research Center (TFHRC) with high performance computing based analysis capabilities in August 2010. The project was established with a new interagency agreement between the Department of Energy and the Department of Transportation to provide collaborative research, development, and benchmarking of advanced three-dimensional computational mechanics analysis methods to the aerodynamics and hydraulics laboratories at TFHRC for a period of five years, beginning in October 2010. The analysis methods employ well benchmarked and supported commercial computational mechanics software. Computational mechanics encompasses the areas of Computational Fluid Dynamics (CFD), Computational Wind Engineering (CWE), Computational Structural Mechanics (CSM), and Computational Multiphysics Mechanics (CMM) applied in Fluid-Structure Interaction (FSI) problems. The major areas of focus of the project are wind and water effects on bridges - superstructure, deck, cables, and substructure (including soil), primarily during storms and flood events - and the risks that these loads pose to structural failure. For flood events at bridges, another major focus of the work is assessment of the risk to bridges caused by scour of stream and riverbed material away from the foundations of a bridge. Other areas of current research include modeling of flow through culverts to improve design allowing for fish passage, modeling of the salt spray transport into bridge girders to address suitability of using weathering steel in bridges, CFD analysis of the operation of the wind tunnel in the TFHRC wind engineering laboratory. This quarterly report documents technical progress on the project tasks for the period of January through March 2012.

  10. Computational mechanics research and support for aerodynamics and hydraulics at TFHRC, year 1 quarter 3 progress report.

    SciTech Connect (OSTI)

    Lottes, S.A.; Kulak, R.F.; Bojanowski, C. (Energy Systems)

    2011-08-26

    The computational fluid dynamics (CFD) and computational structural mechanics (CSM) focus areas at Argonne's Transportation Research and Analysis Computing Center (TRACC) initiated a project to support and compliment the experimental programs at the Turner-Fairbank Highway Research Center (TFHRC) with high performance computing based analysis capabilities in August 2010. The project was established with a new interagency agreement between the Department of Energy and the Department of Transportation to provide collaborative research, development, and benchmarking of advanced three-dimensional computational mechanics analysis methods to the aerodynamics and hydraulics laboratories at TFHRC for a period of five years, beginning in October 2010. The analysis methods employ well-benchmarked and supported commercial computational mechanics software. Computational mechanics encompasses the areas of Computational Fluid Dynamics (CFD), Computational Wind Engineering (CWE), Computational Structural Mechanics (CSM), and Computational Multiphysics Mechanics (CMM) applied in Fluid-Structure Interaction (FSI) problems. The major areas of focus of the project are wind and water loads on bridges - superstructure, deck, cables, and substructure (including soil), primarily during storms and flood events - and the risks that these loads pose to structural failure. For flood events at bridges, another major focus of the work is assessment of the risk to bridges caused by scour of stream and riverbed material away from the foundations of a bridge. Other areas of current research include modeling of flow through culverts to assess them for fish passage, modeling of the salt spray transport into bridge girders to address suitability of using weathering steel in bridges, vehicle stability under high wind loading, and the use of electromagnetic shock absorbers to improve vehicle stability under high wind conditions. This quarterly report documents technical progress on the project tasks for the period of April through June 2011.

  11. Computational mechanics research and support for aerodynamics and hydraulics at TFHRC, year 2 quarter 1 progress report.

    SciTech Connect (OSTI)

    Lottes, S.A.; Bojanowski, C.; Shen, J.; Xie, Z.; Zhai, Y. (Energy Systems); (Turner-Fairbank Highway Research Center)

    2012-04-09

    The computational fluid dynamics (CFD) and computational structural mechanics (CSM) focus areas at Argonne's Transportation Research and Analysis Computing Center (TRACC) initiated a project to support and compliment the experimental programs at the Turner-Fairbank Highway Research Center (TFHRC) with high performance computing based analysis capabilities in August 2010. The project was established with a new interagency agreement between the Department of Energy and the Department of Transportation to provide collaborative research, development, and benchmarking of advanced three-dimensional computational mechanics analysis methods to the aerodynamics and hydraulics laboratories at TFHRC for a period of five years, beginning in October 2010. The analysis methods employ well-benchmarked and supported commercial computational mechanics software. Computational mechanics encompasses the areas of Computational Fluid Dynamics (CFD), Computational Wind Engineering (CWE), Computational Structural Mechanics (CSM), and Computational Multiphysics Mechanics (CMM) applied in Fluid-Structure Interaction (FSI) problems. The major areas of focus of the project are wind and water effects on bridges - superstructure, deck, cables, and substructure (including soil), primarily during storms and flood events - and the risks that these loads pose to structural failure. For flood events at bridges, another major focus of the work is assessment of the risk to bridges caused by scour of stream and riverbed material away from the foundations of a bridge. Other areas of current research include modeling of flow through culverts to improve design allowing for fish passage, modeling of the salt spray transport into bridge girders to address suitability of using weathering steel in bridges, CFD analysis of the operation of the wind tunnel in the TFHRC wind engineering laboratory. This quarterly report documents technical progress on the project tasks for the period of October through December 2011.

  12. Operating characteristics of a 7. 6 mm (0. 30 inch) diameter two-stage light-gas gun

    SciTech Connect (OSTI)

    Susoeff, A R; Hawke, R S; Bowen, P R; Greenwood, D W; Marshall, F R

    1992-07-01

    a series of tests was conducted to determine the operating requirements needed to obtain maximum projectile velocity within the engineering design limits of a two-stage light-gas gun with a 7.6 mm (0.30 inch) diameter bore launch tube. The tests were conducted in a medium vacuum flight range. Previous experience with the gun was used to establish the minimum requirements for optimum efficiency. Two operating parameters, propellant load and drive gas pressure, were varied in order to find an initial optimum operating condition at a conservative propellant load. Propellant load and driver gas pressure were then incrementally increased. This procedure was methodically applied until significant mechanical deformation of a critical gun component took place. This report presents the results of these tests. Projectile velocity was measured to better than 3 percent accuracy using a magnetic induction technique. A 0.485 gram polycarbonate projectile was launched to a velocity of 7.77 km/s during the tests. 13 refs.

  13. Utilization of the MPI Process for in-tank solidification of heel material in large-diameter cylindrical tanks

    SciTech Connect (OSTI)

    Kauschinger, J.L.; Lewis, B.E.

    2000-01-01

    A major problem faced by the US Department of Energy is remediation of sludge and supernatant waste in underground storage tanks. Exhumation of the waste is currently the preferred remediation method. However, exhumation cannot completely remove all of the contaminated materials from the tanks. For large-diameter tanks, amounts of highly contaminated ``heel'' material approaching 20,000 gal can remain. Often sludge containing zeolite particles leaves ``sand bars'' of locally contaminated material across the floor of the tank. The best management practices for in-tank treatment (stabilization and immobilization) of wastes require an integrated approach to develop appropriate treatment agents that can be safely delivered and mixed uniformly with sludge. Ground Environmental Services has developed and demonstrated a remotely controlled, high-velocity jet delivery system termed, Multi-Point-Injection (MPI). This robust jet delivery system has been field-deployed to create homogeneous monoliths containing shallow buried miscellaneous waste in trenches [fiscal year (FY) 1995] and surrogate sludge in cylindrical (FY 1998) and long, horizontal tanks (FY 1999). During the FY 1998 demonstration, the MPI process successfully formed a 32-ton uniform monolith of grout and waste surrogates in about 8 min. Analytical data indicated that 10 tons of zeolite-type physical surrogate were uniformly mixed within a 40-in.-thick monolith without lifting the MPI jetting tools off the tank floor. Over 1,000 lb of cohesive surrogates, with consistencies similar to Gunite and Associated Tank (GAAT) TH-4 and Hanford tank sludges, were easily intermixed into the monolith without exceeding a core temperature of 100 F during curing.

  14. Single-domain magnetic pillar array of 35 nm diameter and 65 Gbits/ik2 density for ultrahigh density quantum magnetic storage

    E-Print Network [OSTI]

    beam nanolithography and electroplating, arrays of Ni pillars on silicon that have a uniform diameter electron beam nanolithography and electroplating. The unique advantage of nanolithography and methanol solution creating a template for the electroplating process. The sample was immersed in a nickel

  15. A comparison of the heat transfer and pressure drop performance of R-134a-lubricant mixtures in different diameter smooth tubes and micro-fin tubes

    SciTech Connect (OSTI)

    Eckels, S.J.; Doerr, T.M.; Pate, M.B.

    1998-10-01

    The average heat transfer coefficients and pressure drops during evaporation and condensation are reported for mixtures of R-134a and an ester lubricant in tubes of 12.7 mm (1/2 in.) outer diameter. The objective of this paper is to evaluate the performance of the R-134a-lubricant mixtures in these tubes and determine the performance benefits of the micro-fin tube. The performance benefits of the tubes with 12.7 mm (1/2 in.) outer diameter are compared to those of smaller tubes with 9.52 mm (3/8 in.) outer diameter. The lubricant used was a 169 SUS penta erythritol ester mixed-acid lubricant. The lubricant concentration was varied from 0--5.1% in the mixture. The average heat transfer coefficients in the 12.7 mm (1/2 in.) micro-fin tube were 50--150% higher than those for the 12.7 mm (1/2 in.) smooth tube, while pressure drops in the micro-fin tube were 5% to 50% higher than in the smooth tube. The addition of lubricant degraded the average heat transfer coefficients in all cases except during evaporation at low lubricant concentrations. Pressure drops were always increased with the addition of lubricant. The experimental results also indicate that tube diameter has some effect on the performance benefits of the micro-fin tube over that of the smooth tube.

  16. UBC Social, Ecological Economic Development Studies (SEEDS) Student Report Alezo Enterprises Inc.: Manufacturer of Wood Products from Small Diameter Douglas Fir Logs

    E-Print Network [OSTI]

    Forest, will minimize costs of shipping raw materials. Staffing requirements are minimal during the first.: Manufacturer of Wood Products from Small Diameter Douglas Fir Logs Terri Anderson, Dianna Embleton, Alfred Lee Inc. has been created by five successful and interested graduates, with the purpose of manufacturing

  17. Machine Design -2 Consider a machined 60mm diameter shaft made of AISI 1020 HR (Sut = 380 MPa at 20C) quenched

    E-Print Network [OSTI]

    Battaglia, Francine

    Machine Design - 2 Consider a machined 60mm diameter shaft made of AISI 1020 HR (Sut = 380 MPa at 20C) quenched steel shown below. The shaft is supported by bearings at the ends. Mounted upon the shaft are two collars through which fluctuating loads are applied as shown. A groove is machined

  18. Sizing DNA Using a Nanometer-Diameter Pore Jiunn B. Heng, Chuen Ho, Taekyung Kim, Rolf Timp, Aleksij Aksimentiev, Yelena V. Grinkova, Stephen Sligar,

    E-Print Network [OSTI]

    Croquette, Vincent

    an electric field is applied across the membrane, a DNA molecule immersed in electrolyte is attracted established through molecular dynamics simulations. By measuring the duration and magnitude of the blocking of the polymer. INTRODUCTION Nanometer diameter pores pervade biology. They are used to regulate the flow of ions

  19. Heat Transfer -2 A pure platinum wire with diameter D = 3 mm and length L = 20 mm is placed outside on a day when air temperature

    E-Print Network [OSTI]

    Virginia Tech

    Heat Transfer - 2 A pure platinum wire with diameter D = 3 mm and length L = 20 mm is placed outside on a day when air temperature T = 10o C. The heat transfer coefficient at the wire's surface h equation that includes all heat transfer mechanisms involved in this problem. Write this energy balance

  20. Single-domain magnetic pillar array of 35 nm diameter and 65 Gbits/ik2 density for ultrahigh density quantum magnetic storage

    E-Print Network [OSTI]

    density quantum magnetic storage Stephen Y Chou, Mark S. Wei, Peter R. Krauss, and Paul 6. FischerSingle-domain magnetic pillar array of 35 nm diameter and 65 Gbits/ik2 density for ultrahigh is 65 Gbits/in.2-over two orders of magnitude greater than the state-of-the-art magnetic storage density

  1. ORF name Gene name Exp1 Exp2 Exp3 Exp4 Exp5 Exp6 Exp7 Median 30C Note 30C Exp8 Exp9 Exp10 Exp11 Exp12 Exp13 Median 14C Note 14C YOL052C-A DDR2 11.7 4.33 17.8 11.48 2.91 2.99 10.34 10.33870994 GOOD 4.687 3.75 5.36 4.359 2.828 3.09 4.05361036 GOOD

    E-Print Network [OSTI]

    Winston, Fred

    Exp12 Exp13 Median 14C Note 14C YOL052C-A DDR2 11.7 4.33 17.8 11.48 2.91 2.99 10.34 10.33870994 GOOD

  2. Angular Diameters of the G Subdwarf $?$ Cassiopeiae A and the K Dwarfs $?$ Draconis and HR 511 from Interferometric Measurements with the CHARA Array

    E-Print Network [OSTI]

    Tabetha S. Boyajian; Harold A. McAlister; Ellyn K. Baines; Douglas R. Gies; Todd Henry; Wei-Chun Jao; David O'Brien; Deepak Raghavan; Yamina Touhami; Theo A. ten Brummelaar; Chris Farrington; P. J. Goldfinger; Laszlo Sturmann; Judit Sturmann; Nils H. Turner; Stephen Ridgway

    2008-04-29

    Using the longest baselines of the CHARA Array, we have measured the angular diameter of the G5 V subdwarf $\\mu$ Cas A, the first such determination for a halo population star. We compare this result to new diameters for the higher metallicity K0 V stars, $\\sigma$ Dra and HR 511, and find that the metal-poor star, $\\mu$ Cas A, has an effective temperature ($T_{\\rm eff}=5297\\pm32$ K), radius ($R=0.791\\pm0.008 R_{\\rm \\odot}$), and absolute luminosity ($L=0.442\\pm0.014 L_{\\rm \\odot}$) comparable to the other two stars with later spectral types. We show that stellar models show a discrepancy in the predicted temperature and radius for $\\mu$ Cas A, and we discuss these results and how they provide a key to understanding the fundamental relationships for stars with low metallicity.

  3. Measured Results for a New Hole-Pattern Annular Gas Seal Incorporating Larger Diameter Holes, Comparisons to Results for a Traditional Hole-Pattern Seal and Predictions

    E-Print Network [OSTI]

    Vannarsdall, Michael Lloyd

    2012-10-19

    C Normalized effective damping [F.t/L] * ijC Normalized direct and cross-coupled stiffness [s] dw Incremental work [J] D Diameter of seal [L] D Direct complex dynamic stiffness [F/L] iD Fourier transformation of displacement [L] E Cross... with increasing preswirl causing the seal to become less stable with increasing preswirl. Cross coupled stiffness increased with increasing running speed. Two clearances: 0.1 mm (4 mils) and 0.2 mm (8 mils) were tested. The results demonstrated...

  4. BRANCH?BASED MODEL FOR THE DIAMETERS OF THE PULMONARY AIRWAYS: ACCOUNTING FOR DEPARTURES FROM SELF?CONSISTENCY AND REGISTRATION ERRORS

    SciTech Connect (OSTI)

    Neradilek, Moni Blazej; Polissar, Nayak; Einstein, Daniel R.; Glenny, Robb W.; Minard, Kevin R.; Carson, James P.; Jiao, Xiangmin; Jacob, Rick E.; Cox, Timothy C.; Postlewait, Ed; Corley, Richard A.

    2012-06-01

    We examine a previously published branch-based approach to modeling airway diameters that is predicated on the assumption of self-consistency across all levels of the tree. We mathematically formulate this assumption, propose a method to test it and develop a more general model to be used when the assumption is violated. We discuss the effect of measurement error on the estimated models and propose methods that account for it. The methods are illustrated on data from MRI and CT images of silicone casts of two rats, two normal monkeys and one ozone-exposed monkey. Our results showed substantial departures from self-consistency in all five subjects. When departures from selfconsistency exist we do not recommend using the self-consistency model, even as an approximation, as we have shown that it may likely lead to an incorrect representation of the diameter geometry. Measurement error has an important impact on the estimated morphometry models and needs to be accounted for in the analysis.

  5. Influence of the Pipe Diameter on the Structure of the Gas-Liquid Interface in a Vertical Two-Phase Pipe Flow

    SciTech Connect (OSTI)

    Prasser, H.-M.; Beyer, M.; Boettger, A.; Carl, H.; Lucas, D.; Schaffrath, A.; Schuetz, P.; Weiss, F.-P.; Zschau, J. [Forschungszentrum Rossendorf (Germany)

    2005-10-15

    Air-water two-phase flow tests in a large vertical pipe of 194.1-mm inner diameter (i.d.) are reported. Close to the outlet of a 9-m-tall test section, two wire-mesh sensors are installed that deliver instantaneous void fraction distributions over the entire cross section with a resolution of 3 mm and 2500 Hz used for fast-flow visualization. Void fraction profiles, gas velocity profiles, and bubble-size distributions were obtained. A comparison to a small pipe of 52.3-mm i.d. (DN50) revealed significant scaling effects. Here, the increase of the airflow rate leads to a transition from bubbly via slug to churn-turbulent flow. This is accompanied by an appearance of a second peak in the bubble-size distribution. A similar behavior was found in the large pipe; though the large bubbles have a significantly larger diameter at identical superficial velocities, the peak is less high but wider. These bubbles move more freely in the large pipe and show more deformations. The shapes of such large bubbles were characterized in three dimensions. They can be rather complicated and far from ideal Taylor bubbles. Also, the small bubble fraction tends to bigger sizes in the large pipe.

  6. Aerodynamics and Heat Transfer Studies of Parameters Specific to the IGCC-Requirements: Endwall Contouring, Leading Edge and Blade Tip Ejection under Rotating Turbine Conditions

    SciTech Connect (OSTI)

    Schobeiri, Meinhard; Han, Je-Chin

    2014-09-30

    This report deals with the specific aerodynamics and heat transfer problematic inherent to high pressure (HP) turbine sections of IGCC-gas turbines. Issues of primary relevance to a turbine stage operating in an IGCC-environment are: (1) decreasing the strength of the secondary flow vortices at the hub and tip regions to reduce (a), the secondary flow losses and (b), the potential for end wall deposition, erosion and corrosion due to secondary flow driven migration of gas flow particles to the hub and tip regions, (2) providing a robust film cooling technology at the hub and that sustains high cooling effectiveness less sensitive to deposition, (3) investigating the impact of blade tip geometry on film cooling effectiveness. The document includes numerical and experimental investigations of above issues. The experimental investigations were performed in the three-stage multi-purpose turbine research facility at the Turbomachinery Performance and Flow Research Laboratory (TPFL), Texas A&M University. For the numerical investigations a commercial Navier-Stokes solver was utilized.

  7. Using Mesoscale Weather Model Output as Boundary Conditions for Atmospheric Large-Eddy Simulations and Wind-Plant Aerodynamic Simulations (Presentation)

    SciTech Connect (OSTI)

    Churchfield, M. J.; Michalakes, J.; Vanderwende, B.; Lee, S.; Sprague, M. A.; Lundquist, J. K.; Moriarty, P. J.

    2013-10-01

    Wind plant aerodynamics are directly affected by the microscale weather, which is directly influenced by the mesoscale weather. Microscale weather refers to processes that occur within the atmospheric boundary layer with the largest scales being a few hundred meters to a few kilometers depending on the atmospheric stability of the boundary layer. Mesoscale weather refers to large weather patterns, such as weather fronts, with the largest scales being hundreds of kilometers wide. Sometimes microscale simulations that capture mesoscale-driven variations (changes in wind speed and direction over time or across the spatial extent of a wind plant) are important in wind plant analysis. In this paper, we present our preliminary work in coupling a mesoscale weather model with a microscale atmospheric large-eddy simulation model. The coupling is one-way beginning with the weather model and ending with a computational fluid dynamics solver using the weather model in coarse large-eddy simulation mode as an intermediary. We simulate one hour of daytime moderately convective microscale development driven by the mesoscale data, which are applied as initial and boundary conditions to the microscale domain, at a site in Iowa. We analyze the time and distance necessary for the smallest resolvable microscales to develop.

  8. Computational mechanics research and support for aerodynamics and hydraulics at TFHRC. Quarterly report January through March 2011. Year 1 Quarter 2 progress report.

    SciTech Connect (OSTI)

    Lottes, S. A.; Kulak, R. F.; Bojanowski, C. (Energy Systems)

    2011-05-19

    This project was established with a new interagency agreement between the Department of Energy and the Department of Transportation to provide collaborative research, development, and benchmarking of advanced three-dimensional computational mechanics analysis methods to the aerodynamics and hydraulics laboratories at the Turner-Fairbank Highway Research Center for a period of five years, beginning in October 2010. The analysis methods employ well-benchmarked and supported commercial computational mechanics software. Computational mechanics encompasses the areas of Computational Fluid Dynamics (CFD), Computational Wind Engineering (CWE), Computational Structural Mechanics (CSM), and Computational Multiphysics Mechanics (CMM) applied in Fluid-Structure Interaction (FSI) problems. The major areas of focus of the project are wind and water loads on bridges - superstructure, deck, cables, and substructure (including soil), primarily during storms and flood events - and the risks that these loads pose to structural failure. For flood events at bridges, another major focus of the work is assessment of the risk to bridges caused by scour of stream and riverbed material away from the foundations of a bridge. Other areas of current research include modeling of flow through culverts to assess them for fish passage, modeling of the salt spray transport into bridge girders to address suitability of using weathering steel in bridges, vehicle stability under high wind loading, and the use of electromagnetic shock absorbers to improve vehicle stability under high wind conditions. This quarterly report documents technical progress on the project tasks for the period of January through March 2011.

  9. Two-phase flow regimes and carry-over in a large-diameter model of a PWR hot leg. Final report

    SciTech Connect (OSTI)

    Hashemi, A.

    1986-04-01

    This report describes a series of tests investigating two-phase flow characterization and carryover in a transparent model of a Babcock and Wilson (B and W) Pressurized Water Reactor (PWR) hot leg geometry. This work was performed, inpart, to support the interpretation of results from the Once-Through Integral System (OTIS) and Multi-loop Integral Test (MIST) facilities. Test conditions were selected to cover a wide range of gas and liquid superficial velocities (0.01 m/s < j/sub g/ < 2 m/s, 0 < j/sub l/ < 0.5 m/s) expected to occur in a prototypical reactor geometry during a small break loss of coolant accident (SBLOCA). Tests at high gas superficial velocities (j/sub g/ > 2 m/s) were also performed for comparison with semi-analytical predictions. Tests were conducted in two different test rigs, one with 10.2-cm (4-inch) diameter pipe, and the other with 30.5-cm (12-inch) diameter pipe. Results include average void fraction, amount of water carryover through the U-bend, transient flow rates and pressure histories, and video movies of the two-phase flow phenomena. Results of the 10.2-cm (4-inch) pipe tests show generally good agreement with the Taitel and Dukler (1) flow regime map for vertical pipes. For the 30.5-cm pipe tests, slug flow was not observed. Instead, as the air flow rate was increased, the flow regime progressed from bubbly to churn-type flow with the presence of large bubbles (approximately 15-cm diameter). The results also indicate that flow regimes and collapsed liquid level are more strongly dependent on air superficial velocity than the water superficial velocity and that the amount of water carryover for a given air flow rate is a strong function of collapsed water level (void fraction). Furthermore, the results show that similar thresholds for breakdown in natural circulation flow exist between the 10.2-cm and 30.5-cm pipe tests for gas and liquid superficial velocities expected in a SBLOCA. 20 refs., 24 figs.

  10. Infrared and visual lunar occultations measurements of stellar diameters and new binary stars detections at the Calar Alto 1.5m telescope

    E-Print Network [OSTI]

    O. Fors; A. Richichi; J. Nunez; A. Prades

    2004-02-03

    We present a program of routine lunar occultations, at optical and near-IR wavelengths, recently started at the 1.5m Spanish telescope at the Calar Alto Observatory. Both a CCD and an infrared array detector are used. The program is aimed mainly at the detection and investigation of binary systems, although results in other areas of stellar research are also anticipated. Occultations are reported for a total of 40 stars. Among these, SAO 164567, SAO 78258 and AG+24 788 have been discovered to be binaries, with projected separations as small as 0.006". Furthermore, binarity is suspected in the case of SAO 78119 and SAO 79251. Additionally, the angular diameter of the late-type giant 30 Psc and of the infrared star V349 Gem have been accurately measured, this latter for the first time. We finally evaluate the instrumentation performance in terms of limiting magnitude and angular resolution, and discuss applications to larger telescopes.

  11. A Study of Production/Injection Data from Slim Holes and Large-Diameter Wells at the Okuaizu Geothermal Field, Tohoku, Japan

    SciTech Connect (OSTI)

    Renner, Joel Lawrence; Garg, Sabodh K.; Combs, Jim

    2002-06-01

    Discharge from the Okuaizu boreholes is accompanied by in situ boiling. Analysis of cold-water injection and discharge data from the Okuaizu boreholes indicates that the two-phase productivity index is about an order of magnitude smaller than the injectivity index. The latter conclusion is in agreement with analyses of similar data from Oguni, Sumikawa, and Kirishima geothermal fields. A wellbore simulator was used to examine the effect of borehole diameter on the discharge capacity of geothermal boreholes with two-phase feedzones. Based on these analyses, it appears that it should be possible to deduce the discharge characteristics of largediameter wells using test data from slim holes with two-phase feeds.

  12. Criticality Safety Study of UF6and UO2F2in 8-in. Inner Diameter Piping

    SciTech Connect (OSTI)

    Elam, K.R.

    2003-10-07

    The purpose of this report is to provide an evaluation of the criticality safety aspects of using up to 8-in.-inner-diameter (ID) piping as part of a system to monitor the {sup 235}U enrichment in uranium hexafluoride (UF{sub 6}) gas both before and after an enrichment down-blending operation. The evaluated operation does not include the blending stage but includes only the monitors and the piping directly associated with the monitors, which are in a separate room from the blending operation. There are active controls in place to limit the enrichment of the blended UF{sub 6} to a maximum of 5 weight percent (wt%) {sup 235}U. Under normal operating conditions of temperature and pressure, the UF{sub 6} will stay in the gas phase and criticality will not be credible. The two accidents of concern are solidification of the UF{sub 6} along with some hydrofluoric acid (HF) and water or moisture ingress, which would cause the UF{sub 6} gas to react and form a hydrated uranyl fluoride (UO{sub 2}F{sub 2}) solid or solution. Of these two types of accidents, the addition of water and formation of UO{sub 2}F{sub 2} is the most reactive scenario and thus limits related to UO{sub 2}F{sub 2} will bound the limits related to UF{sub 6}. Two types of systems are included in the monitoring process. The first measures the enrichment of the approximately 90 wt% enriched UF{sub 6} before it is blended. This system uses a maximum 4-in.-(10.16-cm-) ID pipe, which is smaller than the 13.7-cm-cylinder-diameter subcritical limit for UO{sub 2}F{sub 2} solution of any enrichment as given in Table 1 of American National Standard ANSI/ANS-8.1.1 Therefore, this system poses no criticality concerns for either accident scenario. The second type of system includes two enrichment monitors for lower-enriched UF{sub 6}. One monitors the approximately 1.5 wt% enriched UF{sub 6} entering the blending process, and the second monitors the approximately 5 wt% enriched UF{sub 6} coming out of the blending process. Both use a maximum 8-in.-(20.32-cm-) ID piping, where the length of the larger ID piping is approximately 9.5 m. This diameter of piping is below the 26.6-cm-cylinder-diameter subcritical limit for 5 wt% enriched UO{sub 2}F{sub 2} solutions as given in Table 6 of ANSI/ANS-8.1. Therefore, for up to 5 wt% enriched UF{sub 6}, this piping does not present a criticality concern for either accident scenario. Calculations were performed to determine the enrichment level at which criticality could become a concern in these 8-in.-ID piping sections. Both unreflected and fully water-reflected conditions were considered.

  13. THE RADIO SURFACE-BRIGHTNESS-TO-DIAMETER RELATION FOR GALACTIC SUPERNOVA REMNANTS: SAMPLE SELECTION AND ROBUST ANALYSIS WITH VARIOUS FITTING OFFSETS

    SciTech Connect (OSTI)

    Pavlovic, M. Z.; Urosevic, D.; Arbutina, B. [Department of Astronomy, Faculty of Mathematics, University of Belgrade, Studentski trg 16, 11000 Belgrade (Serbia); Vukotic, B. [Astronomical Observatory, Volgina 7, 11060 Belgrade 38 (Serbia); Goeker, Ue. D., E-mail: marko@math.rs [Physics Department, Bogazici University, Bebek 34342, Istanbul (Turkey)

    2013-01-15

    In this paper, we present new empirical radio surface-brightness-to-diameter ({Sigma}-D) relations for supernova remnants (SNRs) in our Galaxy. We also present new theoretical derivations of the {Sigma}-D relation based on equipartition or on a constant ratio between cosmic rays and magnetic field energy. A new calibration sample of 60 Galactic SNRs with independently determined distances is created. Instead of (standard) vertical regression, used in previous papers, different fitting procedures are applied to the calibration sample in the log {Sigma}-log D plane. Non-standard regressions are used to satisfy the requirement that values of parameters obtained from the fitting of {Sigma}-D and D-{Sigma} relations should be invariant within estimated uncertainties. We impose symmetry between {Sigma}-D and D-{Sigma} due to the existence of large scatter in both D and {Sigma}. Using four fitting methods that treat {Sigma} and D symmetrically, different {Sigma}-D slopes {beta} are obtained for the calibration sample. Monte Carlo simulations verify that the slopes of the empirical {Sigma}-D relation should be determined by using orthogonal regression because of its good performance in data sets with severe scatter. The slope derived here ({beta} = 4.8) is significantly steeper than those derived in previous studies. This new slope is closer to the updated theoretically predicted surface-brightness-diameter slope in the radio range of the Sedov phase. We also analyze the empirical {Sigma}-D relations for SNRs in a dense environment of molecular clouds and for SNRs evolving in the lower-density interstellar medium. Applying new empirical relations to estimate distances of Galactic SNRs results in a dramatically changed distance scale.

  14. Novel techniques and devices for in-situ film coatings of long, small diameter tubes or elliptical and other surface contours

    DOE Public Access Gateway for Energy & Science Beta (PAGES Beta)

    Hershcovitch, Ady; Blaskiewicz, Michael; Brennan, Joseph Michael; Fischer, Wolfram; Liaw, Chong -Jer; Meng, Wuzhang; Todd, Robert; Custer, Art; Dingus, Aaron; Erikson, Mark; et al

    2015-07-30

    In this study, devices and techniques that can, via physical vapor deposition,coat various surface contours or very long small aperture pipes, are described. Recently, a magnetron mole was developed in order to in-situ coat accelerator tube sections of the Brookhaven National Lab relativistic heavy ion collider that have 7.1 cm diameter with access points that are 500 m apart, for copper coat the accelerator vacuum tube in order to alleviate the problems of unacceptable ohmic heating and of electron clouds. A magnetron with a 50 cm long cathode was designed fabricated and successfully operated to copper coat a whole assemblymorecontaining a full-size, stainless steel, cold bore, of the accelerator magnet tubing connected to two types bellows, to which two additional pipes made of accelerator tubing were connected. The magnetron is mounted on a carriage with spring loaded wheels that successfully crossed bellows and adjusted for variations in vacuum tube diameter, while keeping the magnetron centered. Electrical power and cooling water were fed through a cable bundle. The umbilical cabling system, which is enclosed in a flexible braided metal sleeve, is driven by a motorized spool. To increase cathode lifetime, movable magnet package was developed, and thickest possible cathode was made, with a rather challenging target to substrate distance of less than 1.5 cm. Optimized process to ensure excellent adhesion was developed. Coating thickness of 10 ?m Cu passed all industrial tests and even exceeded maximum capability of a 12 kg pull test fixture. Room temperature radio frequency (RF) resistivity measurement indicated that 10 ?m Cu coated stainless steel accelerator tube has conductivity close to copper tubing. Work is in progress to repeat the RF resistivity measurement at cryogenic temperatures. Over 20 years ago, a device using multi axis robotic manipulators controlling separate robotic assemblies resulted in nine-axes of motion combined with conformal shape of the cathodes that can adapt to various curved surface contours was developed and successfully used for depositing optical coating on aircraft canopies. The techniques can be utilized for in situ coating of elliptical and other surface contour RF cavities and long beam pipes with thick superconducting films. Plans are to incorporate ion assisted deposition in those techniques for attaining dense, adherent and defect free coatings.less

  15. Renal Artery Embolization Combined With Radiofrequency Ablation in a Porcine Kidney Model: Effect of Small and Narrowly Calibrated Microparticles as Embolization Material on Coagulation Diameter, Volume, and Shape

    SciTech Connect (OSTI)

    Sommer, C. M., E-mail: christof.sommer@med.uni-heidelberg.de; Kortes, N. [University Hospital Heidelberg, Department of Diagnostic and Interventional Radiology (Germany); Zelzer, S. [German Cancer Research Center, Division of Medical and Biological Informatics (Germany); Arnegger, F. U. [University Hospital Heidelberg, Department of General, Abdominal and Transplantation Surgery (Germany); Stampfl, U.; Bellemann, N. [University Hospital Heidelberg, Department of Diagnostic and Interventional Radiology (Germany); Gehrig, T.; Nickel, F.; Kenngott, H. G. [University Hospital Heidelberg, Department of General, Abdominal and Transplantation Surgery (Germany); Mogler, C.; Longerich, T. [University Hospital Heidelberg, Department of General Pathology (Germany); Meinzer, H. P. [German Cancer Research Center, Division of Medical and Biological Informatics (Germany); Richter, G. M. [Klinikum Stuttgart, Department of Diagnostic and Interventional Radiology (Germany); Kauczor, H. U.; Radeleff, B. A. [University Hospital Heidelberg, Department of Diagnostic and Interventional Radiology (Germany)

    2011-02-15

    The purpose of this study was to evaluate the effect of renal artery embolization with small and narrowly calibrated microparticles on the coagulation diameter, volume, and shape of radiofrequency ablations (RFAs) in porcine kidneys. Forty-eight RFAs were performed in 24 kidneys of 12 pigs. In 6 animals, bilateral renal artery embolization was performed with small and narrowly calibrated microparticles. Upper and lower kidney poles were ablated with identical system parameters. Applying three-dimensional segmentation software, RFAs were segmented on registered 2 mm-thin macroscopic slices. Length, depth, width, volume{sub s}egmented, and volume{sub c}alculated were determined to describe the size of the RFAs. To evaluate the shape of the RFAs, depth-to-width ratio (perfect symmetry-to-lesion length was indicated by a ratio of 1), sphericity ratio (perfect sphere was indicated by a sphericity ratio of 1), eccentricity (perfect sphere was indicated by an eccentricity of 0), and circularity (perfect circle was indicated by a circularity of 1) were determined. Embolized compared with nonembolized RFAs showed significantly greater depth (23.4 {+-} 3.6 vs. 17.2 {+-} 1.8 mm; p < 0.001) and width (20.1 {+-} 2.9 vs. 12.6 {+-} 3.7 mm; p < 0.001); significantly larger volume{sub s}egmented (8.6 {+-} 3.2 vs. 3.0 {+-} 0.7 ml; p < 0.001) and volume{sub c}alculated (8.4 {+-} 3.0 ml vs. 3.3 {+-} 1.1 ml; p < 0.001); significantly lower depth-to-width (1.17 {+-} 0.10 vs. 1.48 {+-} 0.44; p < 0.05), sphericity (1.55 {+-} 0.44 vs. 1.96 {+-} 0.43; p < 0.01), and eccentricity (0.84 {+-} 0.61 vs. 1.73 {+-} 0.91; p < 0.01) ratios; and significantly greater circularity (0.62 {+-} 0.14 vs. 0.45 {+-} 0.16; p < 0.01). Renal artery embolization with small and narrowly calibrated microparticles affected the coagulation diameter, volume, and shape of RFAs in porcine kidneys. Embolized RFAs were significantly larger and more spherical compared with nonembolized RFAs.

  16. Novel techniques and devices for in-situ film coatings of long, small diameter tubes or elliptical and other surface contours

    SciTech Connect (OSTI)

    Hershcovitch, Ady; Blaskiewicz, Michael; Brennan, Joseph Michael; Fischer, Wolfram; Liaw, Chong -Jer; Meng, Wuzhang; Todd, Robert; Custer, Art; Dingus, Aaron; Erikson, Mark; Jamshidi, Nader; Poole, Henry Joe

    2015-07-30

    In this study, devices and techniques that can, via physical vapor deposition,coat various surface contours or very long small aperture pipes, are described. Recently, a magnetron mole was developed in order to in-situ coat accelerator tube sections of the Brookhaven National Lab relativistic heavy ion collider that have 7.1 cm diameter with access points that are 500 m apart, for copper coat the accelerator vacuum tube in order to alleviate the problems of unacceptable ohmic heating and of electron clouds. A magnetron with a 50 cm long cathode was designed fabricated and successfully operated to copper coat a whole assembly containing a full-size, stainless steel, cold bore, of the accelerator magnet tubing connected to two types bellows, to which two additional pipes made of accelerator tubing were connected. The magnetron is mounted on a carriage with spring loaded wheels that successfully crossed bellows and adjusted for variations in vacuum tube diameter, while keeping the magnetron centered. Electrical power and cooling water were fed through a cable bundle. The umbilical cabling system, which is enclosed in a flexible braided metal sleeve, is driven by a motorized spool. To increase cathode lifetime, movable magnet package was developed, and thickest possible cathode was made, with a rather challenging target to substrate distance of less than 1.5 cm. Optimized process to ensure excellent adhesion was developed. Coating thickness of 10 ?m Cu passed all industrial tests and even exceeded maximum capability of a 12 kg pull test fixture. Room temperature radio frequency (RF) resistivity measurement indicated that 10 ?m Cu coated stainless steel accelerator tube has conductivity close to copper tubing. Work is in progress to repeat the RF resistivity measurement at cryogenic temperatures. Over 20 years ago, a device using multi axis robotic manipulators controlling separate robotic assemblies resulted in nine-axes of motion combined with conformal shape of the cathodes that can adapt to various curved surface contours was developed and successfully used for depositing optical coating on aircraft canopies. The techniques can be utilized for in situ coating of elliptical and other surface contour RF cavities and long beam pipes with thick superconducting films. Plans are to incorporate ion assisted deposition in those techniques for attaining dense, adherent and defect free coatings.

  17. Bifunction in Er{sup 3+}/Yb{sup 3+} co-doped BaTi{sub 2}O{sub 5}Gd{sub 2}O{sub 3} glasses prepared by aerodynamic levitation method

    SciTech Connect (OSTI)

    Zhang, Minghui; Yu, Jianding; Pan, Xiuhong; Cheng, Yuxing; Liu, Yan

    2013-11-15

    Graphical abstract: - Highlights: Novel BaTi{sub 2}O{sub 5}Gd{sub 2}O{sub 3} based glasses have been prepared by aerodynamic levitation. The obtained glasses show high thermal stability with T{sub g} = 763.3 C. Er{sup 3+}/Yb{sup 3+} co-doped glasses show strong upconversion based on a two-photon process. Red emission is stronger than green emissions for EBT by high Yb{sup 3+} concentration. Magnetic ions are paramagnetic and the distribution is homogeneous in the glasses. - Abstract: Novel Er{sup 3+}/Yb{sup 3+} co-doped BaTi{sub 2}O{sub 5}Gd{sub 2}O{sub 3} spherical glasses have been fabricated by aerodynamic levitation method. The thermal stability, upconversion luminescence, and magnetic properties of the present glass have been studied. The glasses show high thermal stability with 763.3 C of the onset temperature of the glass transition. Red and green emissions centered at 671 nm, 548 nm and 535 nm are obtained at 980 nm excitation. The upconversion is based on a two-photon process by energy transfer, excited-state absorption, and energy back transfer. Yb{sup 3+} ions are more than Er{sup 3+} ions in the glass, resulting in efficient energy back transfer from Er{sup 3+} to Yb{sup 3+}. So the red emission is stronger than the green emissions. Magnetization curves indicate that magnetic rare earth ions are paramagnetic and the distribution is homogeneous and random in the glass matrix. Aerodynamic levitation method is an efficient way to prepare glasses with homogeneous rare earth ions.

  18. Condensation heat transfer characteristics of R410A-oil mixture in 5 mm and 4 mm outside diameter horizontal microfin tubes

    SciTech Connect (OSTI)

    Huang, Xiangchao; Ding, Guoliang; Hu, Haitao; Zhu, Yu. [Institute of Refrigeration and Cryogenics, Shanghai Jiaotong University, Shanghai 200240 (China); Gao, Yifeng [International Copper Association Shanghai Office, Shanghai 200020 (China); Deng, Bin [Institute of Heat Transfer Technology, Golden Dragon Precise Copper Tube Group Inc., Shanghai 200135 (China)

    2010-10-15

    Condensation heat transfer characteristics of R410A-oil mixture in 5 mm and 4 mm outside diameter horizontal microfin tubes were investigated experimentally. The experimental condensing temperature is 40 C, and nominal oil concentration range is from 0% to 5%. The test results indicate that the presence of oil deteriorates the heat transfer. The deterioration effect is negligible at nominal oil concentration of 1%, and becomes obvious with the increase of nominal oil concentration. At 5% nominal oil concentration, the heat transfer coefficient of R410A-oil mixture is found to have a maximum reduction of 25.1% and 23.8% for 5 mm and 4 mm tubes, respectively. The predictabilities of the existing condensation heat transfer correlations were verified with the experimental data, and Yu and Koyama correlation shows the best predictability. By replacing the pure refrigerant properties with the mixture's properties, Yu and Koyama correlation has a deviation of -15% to + 20% in predicting the local condensation heat transfer coefficient of R410A-oil mixture. (author)

  19. Project W420 Air Sampler Probe Placement Qualification Tests for Four 6-Inch Diameter Stacks: 296-A-25, 296-B-28, 296-S-22, and 296-T-18

    SciTech Connect (OSTI)

    Maughan, A.D.; Glissmeyer, J.A.

    1998-09-30

    The W420 project covers the upgrading of effluent monitoring systems at six ventilation exhaust stacks in tank-farm facilities at the U.S. Department of Energy's Hanford Site. The discharge stacks of five of the six systems will be completely replaced. Four of these (296-A-25, 296-B-28, 296-S-22, and 296-T-18) will be of the same size, 6-inches in diameter and about 12-ft high. This report documents tests that were conducted to verify that these four stacks meet the applicable regulatory criteria regarding the placement of the air sampling probe. These criteria ensure that the contaminants in the stack are well mixed with the airflow at the location of the probe such that the extracted sample represents the whole. There are also criteria addressing the transport of the sample to the collection device. These are not covered in this report, but will need to be addressed later. These tests were conducted by Pacific Northwest National Laboratory on a full-scale model of the 6-inch stick. The sequence of tests addresses the acceptability of the flow angle relative to the probe and the uniformity of air velocity and gaseous and particle tracers in the cross section of the stack. All tests were successful, and all acceptance criteria were met.

  20. Introduction to AERODYNAMICS Aerodynamics is an applied science to learn

    E-Print Network [OSTI]

    Leu, Tzong-Shyng "Jeremy"

    forces on wind turbine, building (bridge), sports (bicycle, baseball) - Hydrodynamic forces on ships forces (lift, drag), moments and center of pressure on flying objects (airfoil, airplanes, birds) - Wind as the instantaneous velocity of the center of the m Defining a fluid particle as a small mass of m

  1. APPLIED AERODYNAMICS Aerodynamics is an applied science to learn

    E-Print Network [OSTI]

    Leu, Tzong-Shyng "Jeremy"

    on flying objects (insects, birds, airplanes, missiles) - Wind forces on building, cars, sports (ski the application of a shear (tangential) stress. No matter how small the shear stress may be, a fluid will deform the nature of the fluid. VALID, whenever the small

  2. Intelligent scraping experience using ultrasonics in two 60in./56in. dual diameter 100 km seawater transmission pipelines in Saudi Arabia

    SciTech Connect (OSTI)

    Bird, A.F.; Chu, K.S.

    1995-10-01

    Saudi ARAMCO`s two 60in./56in. (1524/1422 mm) diameter Seawater Injection Pipelines used for secondary oil recovery stretch from the Seawater Treatment Plant across the Arabian Desert for a distance of approximately 100 kilometers. Both lines were put into operation in mid 1978 using over the ditch Plicoflex tape wrap as a means of protection against external corrosion. A significant portion of both pipelines (32 km of each line) runs through Subkha (salty moist) areas. A series of test hole evaluations in 1989 indicated moderate to sever external corrosion particularly in Subkha which necessitated sleeving and external coating application. In 1991 a series of leaks, four (4) in total over a period of two (2) months occurred in Pipeline {number_sign}2 due to external corrosion. This suggested that the line(s) were in urgent need of at least partial replacement or major rehabilitation. Prior to making a final decision on partial replacement it was decided to run an Intelligent Scraper in both pipelines to ascertain both internal and external pipeline conditions. An Ultrasonic Scraper the largest of it`s kind in the world, similar to what was used in the Alyeska Pipeline was developed and successfully run in both pipelines in February 1993. This paper discusses the pipeline history, test hole evaluations, Intelligent Scraping experiences, field evaluation for anomaly verification, and repair of approximately 120 locations as identified by the Intelligent Scraping run. The Intelligent Scraping evaluation played a major role in the cancellation of partial pipeline replacement with cost savings estimated $30 MM.

  3. On the structurization of coal dust precipitations and their influence on aerodynamic resistance by granulated mediums in air filters at nuclear power plants

    E-Print Network [OSTI]

    Neklyudov, I M; Fedorova, L I; Poltinin, P Ya

    2012-01-01

    The processes of structurization of dust precipitations in granulated filtering mediums, formed by the monolithic glass spherical granules with the diameters of 2mm and 3mm, are re-searched. The distinctions between the distributions of filtered coal dust masses in the air filters with cylindrical granules and the air filters with spherical granules, are found. The influences by the filtered dust masses on the air resistance of both the air filters with the cylindrical granules and the air filters with the spherical granules are described. The conclusions on a possibility of the use of various chemical adsorbents with different geometric forms and volumetric dimensions to improve the filtering properties of granulated filtering mediums in air filters at nuclear power plants are formulated.

  4. On the structurization of coal dust precipitations and their influence on aerodynamic resistance by granulated mediums in air filters at nuclear power plants

    E-Print Network [OSTI]

    I. M. Neklyudov; O. P. Ledenyov; L. I. Fedorova; P. Ya. Poltinin

    2012-07-02

    The processes of structurization of dust precipitations in granulated filtering mediums, formed by the monolithic glass spherical granules with the diameters of 2mm and 3mm, are re-searched. The distinctions between the distributions of filtered coal dust masses in the air filters with cylindrical granules and the air filters with spherical granules, are found. The influences by the filtered dust masses on the air resistance of both the air filters with the cylindrical granules and the air filters with the spherical granules are described. The conclusions on a possibility of the use of various chemical adsorbents with different geometric forms and volumetric dimensions to improve the filtering properties of granulated filtering mediums in air filters at nuclear power plants are formulated.

  5. Aerodynamic Lightweight Cab Structure Components

    Office of Energy Efficiency and Renewable Energy (EERE)

    2013 DOE Hydrogen and Fuel Cells Program and Vehicle Technologies Program Annual Merit Review and Peer Evaluation Meeting

  6. Micro-unmanned aerodynamic vehicle

    DOE Patents [OSTI]

    Reuel, Nigel (Rio Rancho, NM); Lionberger, Troy A. (Ann Arbor, MI); Galambos, Paul C. (Albuquerque, NM); Okandan, Murat (Albuquerque, NM); Baker, Michael S. (Albuquerque, NM)

    2008-03-11

    A MEMS-based micro-unmanned vehicle includes at least a pair of wings having leading wing beams and trailing wing beams, at least two actuators, a leading actuator beam coupled to the leading wing beams, a trailing actuator beam coupled to the trailing wing beams, a vehicle body having a plurality of fulcrums pivotally securing the leading wing beams, the trailing wing beams, the leading actuator beam and the trailing actuator beam and having at least one anisotropically etched recess to accommodate a lever-fulcrum motion of the coupled beams, and a power source.

  7. Optimized Active Aerodynamic Blade Control

    Broader source: All U.S. Department of Energy (DOE) Office Webpages (Extended Search)

    AFDC Printable Version Share this resource Send a link to EERE: Alternative Fuels Data Center Home Page to someone by E-mail Share EERE: Alternative Fuels Data Center Home Page on Facebook Tweet about EERE: Alternative Fuels Data Center Home Page on Twitter Bookmark EERE: Alternative Fuels Data Center Homesum_a_epg0_fpd_mmcf_m.xls" ,"Available from WebQuantityBonneville Power Administration wouldMass mapSpeeding access toOctober 1996TechnologiesDistribution, andSpectroscopy ofOptimized

  8. Neo Aerodynamic | Open Energy Information

    Open Energy Info (EERE)

    AFDC Printable Version Share this resource Send a link to EERE: Alternative Fuels Data Center Home Page to someone by E-mail Share EERE: Alternative Fuels Data Center Home Page on Facebook Tweet about EERE: Alternative Fuels Data Center Home Page on Twitter Bookmark EERE: Alternative Fuels Data Center Home Page on Google Bookmark EERE: Alternative Fuels Data Center Home Page on QA:QA J-E-1 SECTION J APPENDIXsourceII Jump to: navigation,National Marine FisheriesPolicyNedPowerNellis

  9. A truck has a fuel tank which is a 20 inch diameter cylinder resting on its rounded side. The driver notices that his fuel gauge is no longer giving the correct readings, so he has to improvise. He places a

    E-Print Network [OSTI]

    Lega, Joceline

    A truck has a fuel tank which is a 20 inch diameter cylinder resting on its rounded side. The driver notices that his fuel gauge is no longer giving the correct readings, so he has to improvise. He to the bottom. He pulls the measuring stick out and finds that the height of the fuel is 6 inches. What fraction

  10. Section 5: Expected Value; Percentiles, Median, and Mode

    E-Print Network [OSTI]

    2014-09-27

    Sep 30, 2014 ... Smith finds the carnival game over-under-seven irresistible. The game involves the random toss of two fair dice. If a player bets 1 on over...

  11. The Online Median Problem Ramgopal R. Mettu C. Greg Plaxton

    E-Print Network [OSTI]

    Mettu, Ramgopal

    @cs.utexas.edu. The second author is presently on leave at Akamai Techologies, Inc., Cambridge, MA 02139. #12; 1 Introduction

  12. The Online Median Problem Ramgopal R. Mettu C. Greg Plaxton

    E-Print Network [OSTI]

    Mettu, Ramgopal

    on leave at Akamai Techologies, Inc., Cambridge, MA 02139. #12;1 Introduction Suppose we wish to open a new

  13. Stable roommates matchings, mirror posets, median graphs, and the local/global median phenomenon in stable matchings

    E-Print Network [OSTI]

    Cheng, Christine

    rise to mirror posets and vice versa, and mirror posets give rise to SR stable matchings and vice versa to as the bipartite version of SR, is the stable marriage problem (SM). There are n men and n women each of whom ranks-0830678. 1 #12;preference list, append an arbitrary ordering of the other men; do the same for the women

  14. Stable roommates matchings, mirror posets, median graphs, and the local/global median phenomenon in stable matchings

    E-Print Network [OSTI]

    Cheng, Christine

    rise to mirror posets and vice versa, and mirror posets give rise to SR stable matchings and vice versa problem (SM). There are n men and n women each of whom ranks participants from the opposite sex only the same for the women. It is straightforward to check that both instances have exactly the same stable

  15. Large Diameter Lasing Tube Cooling Arrangement

    DOE Patents [OSTI]

    Hall, Jerome P.; Alger, Terry W.; Anderson, Andrew T.; Arnold, Philip A.

    2004-05-18

    A cooling structure (16) for use inside a ceramic cylindrical tube (11) of a metal vapor laser (10) to cool the plasma in the tube (11), the cooling structure (16) comprising a plurality of circular metal members (17,31) and mounting members (18, 34) that position the metal members (17,31) coaxially in the tube (11) to form an annular lasing volume, with the metal members (17, 31) being axially spaced from each other along the length of the tube (11) to prevent the metal members from shorting out the current flow through the plasma in the tube (11) and to provide spaces through which the heat from localized hot spots in the plasma may radiate to the other side of the tube (11).

  16. The diameter of the world wide web

    E-Print Network [OSTI]

    Reka Albert; Hawoong Jeong; Albert-Laszlo Barabasi

    1999-09-10

    Despite its increasing role in communication, the world wide web remains the least controlled medium: any individual or institution can create websites with unrestricted number of documents and links. While great efforts are made to map and characterize the Internet's infrastructure, little is known about the topology of the web. Here we take a first step to fill this gap: we use local connectivity measurements to construct a topological model of the world wide web, allowing us to explore and characterize its large scale properties.

  17. Tightening procedures for large diameter anchor bolts

    E-Print Network [OSTI]

    Abraham, Ryan Charles

    1997-01-01

    judgment concerning how tight to tighten the nuts on the anchor bolt system. Recent bolt failures have raised concerns about nut tightening procedures. When the nuts of a double nut system are not tightened sufficiently, fatigue loading, and even impact...

  18. Y-12 Uranium Exposure Study

    SciTech Connect (OSTI)

    Eckerman, K.F.; Kerr, G.D.

    1999-08-05

    Following the recent restart of operations at the Y-12 Plant, the Radiological Control Organization (RCO) observed that the enriched uranium exposures appeared to involve insoluble rather than soluble uranium that presumably characterized most earlier Y-12 operations. These observations necessitated changes in the bioassay program, particularly the need for routine fecal sampling. In addition, it was not reasonable to interpret the bioassay data using metabolic parameter values established during earlier Y-12 operations. Thus, the recent urinary and fecal bioassay data were interpreted using the default guidance in Publication 54 of the International Commission on Radiological Protection (ICRP); that is, inhalation of Class Y uranium with an activity median aerodynamic diameter (AMAD) of 1 {micro}m. Faced with apparently new workplace conditions, these actions were appropriate and ensured a cautionary approach to worker protection. As additional bioassay data were accumulated, it became apparent that the data were not consistent with Publication 54. Therefore, this study was undertaken to examine the situation.

  19. Cell diameter measurements obtained with a handheld cell counter could be used as a surrogate marker of G2/M arrest and apoptosis in colon cancer cell lines exposed to SN-38

    SciTech Connect (OSTI)

    Tahara, Makiko; Inoue, Takeshi; Fujii, Hirofumi; Kotake, Kenjiro; Sugano, Kokichi

    2013-05-17

    Highlights: Chemo-sensitivity to SN-38 was assayed by the automated cell counter. Colon cancer cell line, HCT116 cells were more sensitive to SN-38 than HT29 cells. Increase of cell size reflects G2/M arrest. Appearance of small particles indicates cell apoptosis. -- Abstract: In vitro assessment of chemosensitivity are important for experiments evaluating cancer therapies. The Scepter 2.0 cell counter, an automated handheld device based on the Coulter principle of impedance-based particle detection, enables the accurate discrimination of cell populations according to cell size and volume. In this study, the effects of SN-38, the active metabolite of irinotecan, on the colon cancer cell lines HCT116 and HT29 were evaluated using this device. The cell count data obtained with the Scepter counter were compared with those obtained with the {sup 3}H-thymidine uptake assay, which has been used to measure cell proliferation in many previous studies. In addition, we examined whether the changes in the size distributions of these cells reflected alterations in the frequency of cell cycle arrest and/or apoptosis induced by SN-38 treatment. In our experiments using the Scepter 2.0 cell counter, the cell counts were demonstrated to be accurate and reproducible measure and alterations of cell diameter reflected G2/M cell cycle arrest and apoptosis. Our data show that easy-to-use cell counting tools can be utilized to evaluate the cell-killing effects of novel treatments on cancer cells in vitro.

  20. Uranium mill ore dust characterization

    SciTech Connect (OSTI)

    Knuth, R.H.; George, A.C.

    1980-11-01

    Cascade impactor and general air ore dust measurements were taken in a uranium processing mill in order to characterize the airborne activity, the degree of equilibrium, the particle size distribution and the respirable fraction for the /sup 238/U chain nuclides. The sampling locations were selected to limit the possibility of cross contamination by airborne dusts originating in different process areas of the mill. The reliability of the modified impactor and measurement techniques was ascertained by duplicate sampling. The results reveal no significant deviation from secular equilibrium in both airborne and bulk ore samples for the /sup 234/U and /sup 230/Th nuclides. In total airborne dust measurements, the /sup 226/Ra and /sup 210/Pb nuclides were found to be depleted by 20 and 25%, respectively. Bulk ore samples showed depletions of 10% for the /sup 226/Ra and /sup 210/Pb nuclides. Impactor samples show disequilibrium of /sup 226/Ra as high as +-50% for different size fractions. In these samples the /sup 226/Ra ratio was generally found to increase as particle size decreased. Activity median aerodynamic diameters of the airborne dusts ranged from 5 to 30 ..mu..m with a median diameter of 11 ..mu..m. The maximum respirable fraction for the ore dusts, based on the proposed International Commission on Radiological Protection's (ICRP) definition of pulmonary deposition, was < 15% of the total airborne concentration. Ore dust parameters calculated for impactor duplicate samples were found to be in excellent agreement.

  1. Cyclone aerosol sampling and particle deposition in tubing elements following elbow bends

    E-Print Network [OSTI]

    Wente, William Baker

    1995-01-01

    Dns Da d, d0 Dp Cunningham's correction factor for an aerodynamic particle Cunninghain's correction concentration of the sodium fluoroscein collected at the exit from the system concentration of particles penetrating through the cyclone... Cunningham's correction factor for a particle reference particle concentration concetration of the sodium fluoroscein collected at the inlet to the system cutpoint diameter aerodynamic equivalent diameter cyclone body diameter cyclone outlet tube...

  2. Freight Wing & Aerodynamic Fairings | Department of Energy

    Office of Energy Efficiency and Renewable Energy (EERE) Indexed Site

    Savings Reduces fuel consumption by 7% with use of second-generation belly fairing alone. Emission Reduction Reduces emissions of combustion products, including particulates, SOx,...

  3. SUCCESSES AND CHALLENGES IN COMPUTATIONAL AERODYNAMICS

    E-Print Network [OSTI]

    Jameson, Antony

    of linearized supersonic flow [ Z ] . These methods required simplifying assumptions of various kinds, and could, which will enable designers to produce better airplanes. Second there is the possibility of using supersonic flow [7]. The seventies saw widespread efforts to develop methods of predicting transonic flows

  4. Computational Aerodynamics for Aircraft Design Antony Jameson

    E-Print Network [OSTI]

    Jameson, Antony

    translate into substantial savings in operational costs. Therefore, the operating efficiency of an airplane change in the flow. This occurs when embedded pockets of supersonic flow appear, generally terminating's theory of linearized supersonic flow (2). These methods, however, required simplifying assumptions

  5. Airfoil Optimization Using Practical Aerodynamic Design Requirements

    E-Print Network [OSTI]

    Zingg, David W.

    aviation are of public concern with regard to climate change, and rising jet fuel prices are negatively impacting pro ts of commercial carriers, the design objective of improving aircraft fuel ef ciency

  6. CFD Calculations of S809 Aerodynamic Characteristics

    Broader source: All U.S. Department of Energy (DOE) Office Webpages (Extended Search)

    AFDC Printable Version Share this resource Send a link to EERE: Alternative Fuels Data Center Home Page to someone by E-mail Share EERE: Alternative Fuels Data Center Home Page on Facebook Tweet about EERE: Alternative Fuels Data Center Home Page on Twitter Bookmark EERE: Alternative Fuels Data Center Homesum_a_epg0_fpd_mmcf_m.xls" ,"Available from WebQuantity ofkandz-cm11 OutreachProductswsicloudwsiclouddenDVA N C E D B L OBransenBusinessInitial Validation'IU" 9CERTIFIED P.

  7. This study describes a novel multisite recording probe with linear arrangement of recording sites. It is build from a 30cm long, 650m diameter stainless steel rod featuring 31 microelectrodes on the side of its business end and a conical tip. Recording

    E-Print Network [OSTI]

    Lbeck, Universitt zu

    of recording sites. It is build from a 30cm long, 650m diameter stainless steel rod featuring 31 in any ways. 2. MATERIALS AND METHODS 2.1. Multisite probe fabrication A thin stainless steel tube Activity of neurons across different layers. Keywords: Multsite neuronal recording, steel probe

  8. Microsoft Word - KCP Final EA Draft 042913 CLEAN for Concurrence...

    National Nuclear Security Administration (NNSA)

    2.5 particulate matter with an aerodynamic diameter of 2.5 micrometers or less RCRA Resource Conservation and Recovery Act of 1976 SHPO State Historic Preservation Office SWMU...

  9. Single-ultrafine-particle mass spectrometer development and application

    E-Print Network [OSTI]

    Glagolenko, Stanislav Yurievich

    2004-11-15

    ., 1997], LAMPAS-2 [Trimborn et al., 2000] and SPLAT [Schneider et al., 2004] instruments use light scattering to detect particles, and the aerodynamic diameter is determined from the particle time of flight between two points. The main disadvantage... of the optical techniques is that particles too small to be detected by light scattering (roughly, smaller than 200 nm in diameter) cannot be analyzed. To overcome this limitation, an aerodynamic focusing mechanism was implemented in the RSMS-II instrument...

  10. GUIDE TO CALCULATING TRANSPORT EFFICIENCY OF AEROSOLS IN OCCUPATIONAL AIR SAMPLING SYSTEMS

    SciTech Connect (OSTI)

    Hogue, M.; Hadlock, D.; Thompson, M.; Farfan, E.

    2013-11-12

    This report will present hand calculations for transport efficiency based on aspiration efficiency and particle deposition losses. Because the hand calculations become long and tedious, especially for lognormal distributions of aerosols, an R script (R 2011) will be provided for each element examined. Calculations are provided for the most common elements in a remote air sampling system, including a thin-walled probe in ambient air, straight tubing, bends and a sample housing. One popular alternative approach would be to put such calculations in a spreadsheet, a thorough version of which is shared by Paul Baron via the Aerocalc spreadsheet (Baron 2012). To provide greater transparency and to avoid common spreadsheet vulnerabilities to errors (Burns 2012), this report uses R. The particle size is based on the concept of activity median aerodynamic diameter (AMAD). The AMAD is a particle size in an aerosol where fifty percent of the activity in the aerosol is associated with particles of aerodynamic diameter greater than the AMAD. This concept allows for the simplification of transport efficiency calculations where all particles are treated as spheres with the density of water (1 g?cm-3). In reality, particle densities depend on the actual material involved. Particle geometries can be very complicated. Dynamic shape factors are provided by Hinds (Hinds 1999). Some example factors are: 1.00 for a sphere, 1.08 for a cube, 1.68 for a long cylinder (10 times as long as it is wide), 1.05 to 1.11 for bituminous coal, 1.57 for sand and 1.88 for talc. Revision 1 is made to correct an error in the original version of this report. The particle distributions are based on activity weighting of particles rather than based on the number of particles of each size. Therefore, the mass correction made in the original version is removed from the text and the calculations. Results affected by the change are updated.

  11. Investigation of an empirical methodology for linking value of time with census tract median income

    E-Print Network [OSTI]

    Stockton, William Radney

    2009-05-15

    This research examines a new methodology for prospectively estimating the willingness of travelers to use a toll road by combining travel time saved with the income of the prospective customer base. The purpose of the ...

  12. Most Frequently Selected Fields, With Median Salaries http://www.stat.cornell.edu/mps/

    E-Print Network [OSTI]

    Keinan, Alon

    statistical programming and software, databases, high performance computing as it relates to statistics

  13. Most Frequently Selected Fields, With Median Salaries http://stat.cornell.edu/academics/mps

    E-Print Network [OSTI]

    Keinan, Alon

    statistical programming and software, databases, high performance computing as it relates to statistics

  14. Distribution of the daily F0F sub 2 about the monthly median

    SciTech Connect (OSTI)

    Sowers, M.W.; PoKempner, M.

    1990-05-01

    Data from 21 ionospheric sounding stations in the northern and southern hemispheres were used to characterize the day-to-day variation in the critical frequency of the F2 layer of the ionosphere. Variability in the critical frequencies are analyzed monthly and diurnally for quiet magnetic conditions during both low and high solar periods. In addition, variations in the F2 layer critical frequency are presented for active magnetic conditions during equinox periods. Tables of variabilities for each ten degree increment in magnetic latitude are also provided in the report. The dependence of variations in the critical frequency with the solar cycle index IG12 is also discussed.

  15. South Florida Sun-Sentinel.com Census shows another decline in median income

    E-Print Network [OSTI]

    Fernandez, Eduardo

    's official poverty rate was 15 percent, up a percent from a year earlier when the recession officially ended. That means almost 3 million more Americans were living in poverty in 2010, the Census Bureau reported. It was the fourth annual increase and the largest number of poor people in the 52 years the poverty estimates have

  16. Reliable p-median facility location problem: two-stage robust models ...

    E-Print Network [OSTI]

    2012-12-18

    constraint Generation Method. Technical Report. submitted. Zhao, L., Zeng, B., 2010. Robust Unit Commitment Problem with Demand Response and Wind.

  17. Spatially assisted down-track median filter for GPR image post-processing

    DOE Patents [OSTI]

    Paglieroni, David W; Beer, N Reginald

    2014-10-07

    A method and system for detecting the presence of subsurface objects within a medium is provided. In some embodiments, the imaging and detection system operates in a multistatic mode to collect radar return signals generated by an array of transceiver antenna pairs that is positioned across the surface and that travels down the surface. The imaging and detection system pre-processes the return signal to suppress certain undesirable effects. The imaging and detection system then generates synthetic aperture radar images from real aperture radar images generated from the pre-processed return signal. The imaging and detection system then post-processes the synthetic aperture radar images to improve detection of subsurface objects. The imaging and detection system identifies peaks in the energy levels of the post-processed image frame, which indicates the presence of a subsurface object.

  18. Somatosensory System Deficits in Schizophrenia Revealed by MEG during a Median-Nerve Oddball Task

    E-Print Network [OSTI]

    2010-01-01

    P, Clarke JM, Heit G, Marinkovic K, Devaux B, Vignal JP,94:229250 Halgren E, Marinkovic K, Chauvel P (1998)

  19. NMDOT Application for Permit to Construct an Access or Median Opening on

    Open Energy Info (EERE)

    AFDC Printable Version Share this resource Send a link to EERE: Alternative Fuels Data Center Home Page to someone by E-mail Share EERE: Alternative Fuels Data Center Home Page on Facebook Tweet about EERE: Alternative Fuels Data Center Home Page on Twitter Bookmark EERE: Alternative Fuels Data Center Home Page on Google Bookmark EERE: Alternative Fuels Data Center Home Page on QA:QAsource History ViewMayo, Maryland: EnergyInformationOliver,Minnesota:EnergyNARI| Open Energy26.2| OpenPublic

  20. Table B2. Summary Table: Totals and Medians of Floorspace, Number of Workers,

    U.S. Energy Information Administration (EIA) Indexed Site

    AFDC Printable Version Share this resource Send a link to EERE: Alternative Fuels Data Center Home Page to someone by E-mail Share EERE: Alternative Fuels Data Center Home Page on Facebook Tweet about EERE: Alternative Fuels Data Center Home Page on Twitter Bookmark EERE: Alternative Fuels Data Center Home Page on Google Bookmark EERE: AlternativeMonthly","10/2015"Monthly","10/2015" ,"Release7CubicthroughtheSeptember 24,4,630.22Primary Consumption6.9. Energy.

  1. New structural systems in small-diameter round timber

    E-Print Network [OSTI]

    Bukauskas, Aurimas (Aurimas M.)

    2015-01-01

    Trees, when used as structural elements in their natural, round form, are up to five times stronger than the largest piece of dimensioned lumber they could yield. Additionally, these whole-timbers have a lower effective ...

  2. Periodic Holes with 10 nm Diameter Produced by Grazing Ar+

    E-Print Network [OSTI]

    Metzger, Robert M.

    acid solution at 40 V at 5 C for at least 1 day.10,11 A homogeneous U-shaped barrier oxide layer, 20

  3. Selection of powder factor in large diameter blastholes

    SciTech Connect (OSTI)

    Eloranta, J.

    1995-12-31

    This paper documents the relationship between material handling and processing costs compared to blasting cost. The old adage, The cheapest crushing is done in the pit, appears accurate in this case study. Comparison of the accumulated cost of: powder, selected wear materials and electricity; indicate a strong, inverse correlation with powder factor (lbs powder/long ton of rock). In this case, the increased powder cost is more than offset by electrical savings alone. Measurable, overall costs decline while shovel and crusher productivity rise by about 5% when powder factor rises by 15%. These trends were previously masked by the effects of: weather, ore grade fluctuations and accounting practices. Attempts to correlate increased powder factor to: wear materials in the crushing plant and to shovel hoist rope life have not shown the same benefit.

  4. Modelling Hop-Constrained and Diameter-Constrained Minimum ...

    E-Print Network [OSTI]

    2008-03-05

    arc sets [Si,Si+1] and then it would contain at least H + 1 arcs which is a contradiction. Thus ... set Si to one of the sets Si+2,...,SH+1. .... However, a simple exam-.

  5. Diameter-Refined Metallic Carbon Nanotubes as Optically Tunable Transparent

    Broader source: All U.S. Department of Energy (DOE) Office Webpages (Extended Search)

    AFDC Printable Version Share this resource Send a link to EERE: Alternative Fuels Data Center Home Page to someone by E-mail Share EERE: Alternative Fuels Data Center Home Page on Facebook Tweet about EERE: Alternative Fuels Data Center Home Page on Twitter Bookmark EERE: Alternative Fuels Data Center Homesum_a_epg0_fpd_mmcf_m.xls" ,"Available from WebQuantity ofkandz-cm11 Outreach Home Room NewsInformation Current HAB Packet HanfordDOEDanielDeSmallDevelopment ofBrowse by Topic

  6. Synthesis of very small diameter silica nanofibers using sound waves

    Office of Scientific and Technical Information (OSTI)

    AFDC Printable Version Share this resource Send a link to EERE: Alternative Fuels Data Center Home Page to someone by E-mail Share EERE: Alternative Fuels Data Center Home Page on Facebook Tweet about EERE: Alternative Fuels Data Center Home Page on Twitter Bookmark EERE: Alternative Fuels Data Center Homesum_a_epg0_fpd_mmcf_m.xls" ,"Available from WebQuantity of NaturalDukeWakefieldSulfateSciTechtail. (Conference)Feedback System inStatusandArticle) |HydrogenMetathesiswith ppm

  7. Relationship of Oak Seedling HeightRelationship of Oak Seedling Height and Diameter with Bottomlandand Diameter with Bottomland

    E-Print Network [OSTI]

    Gray, Matthew

    %) Protection & Restoration Clean Water Act (1975) Swampbuster Provision Food Security Act WRP and CRP habitat Timber production Environmental Nutrient cycling Floodwater storage Improve water-7) 1 m high levees Water control structures Elevation gradient (NE to SW) South Fork

  8. SANDIA REPORTSAND78-1737 q Unlimited Release UC-60 Printed September 1978

    E-Print Network [OSTI]

    -metre Darrieus vertical-axis wind turbine was field-tested at the Sandia Laboratories wind-turbine site of the 17 Meter Diameter Darrieus Wind Turbine Mark H. Worstell Prepared by Sandia National Laboratories January 1979 AERODYNAMIC PERFORMANCE OF THE 17-METRE-DIAMETER DARRIEUS WIND TURBINE Mark H. Worstell

  9. The power balance method For aerodynamic performance assessment

    E-Print Network [OSTI]

    Sato, Sho, Ph. D. Massachusetts Institute of Technology

    2012-01-01

    This thesis describes the use of the power balance method for performance estimation of aircraft configurations. In this method, mechanical power production and mechanical power consumption of the aircraft are balanced, ...

  10. Large-Eddy Simulation of Wind-Plant Aerodynamics: Preprint

    SciTech Connect (OSTI)

    Churchfield, M. J.; Lee, S.; Moriarty, P. J.; Martinez, L. A.; Leonardi, S.; Vijayakumar, G.; Brasseur, J. G.

    2012-01-01

    In this work, we present results of a large-eddy simulation of the 48 multi-megawatt turbines composing the Lillgrund wind plant. Turbulent inflow wind is created by performing an atmospheric boundary layer precursor simulation and turbines are modeled using a rotating, variable-speed actuator line representation. The motivation for this work is that few others have done wind plant large-eddy simulations with a substantial number of turbines, and the methods for carrying out the simulations are varied. We wish to draw upon the strengths of the existing simulations and our growing atmospheric large-eddy simulation capability to create a sound methodology for performing this type of simulation. We have used the OpenFOAM CFD toolbox to create our solver.

  11. Luminescence imaging for aerodynamic temperature and pressure measurements

    SciTech Connect (OSTI)

    Gallery, J.M.

    1993-01-01

    A luminescent temperature sensitive paint containing the molecule rhodamine B base (rhBb) is described whose emission intensity can be monitored by video camera to produce qualitative and quantitative two dimensional surface temperature maps. This paint was designed for use with the pressure sensitive paint containing platinum octaethylporphyrin (PtOEP), but is also a useful tool when used alone in the measurement of heat flow, boundary layer transition, and quantitative surface temperature during wind tunnel studies. The ability of the rhBb paint to produce a continuous temperature map makes it possible to locate structures in the temperature field on an airfoil that are otherwise undetected by surface mounted thermocouples spaced a finite distance apart. A dual temperature/pressure sensitive paint was investigated with both the rhBb and PtOEP dyes incorporated into the silicone polymer paint base of the pressure sensor. Photodegradation and batch variations in the polymer were found to compromise the calibration parameters of the PtOEP paint and therefore the accuracy of pressure predictions. Suggestions are made for improving the prediction ability of the paint. The molecule europium(III) thenoyltrifluoroacetonate (EuTTA) is also discussed as a temperature sensor for a two layer temperature/pressure paint. EuTTA can not be directly incorporated into the silicone paint base of the PtOEP paint (as the rhBp paint can), but performs well in non-oxygenpermeable coatings. Benefits of the EuTTA temperature paint include: (1) decreased photodegradation, (2) very bright luminescence intensity, and (3) long luminescent lifetime (several hundred microseconds). The long lifetime facilitates lifetime imaging, a technique currently under development as an alternative detection method where luminescent lifetimes rather than emission intensity are related to temperature and pressure.

  12. Rarefaction Effects in Hypersonic Aerodynamics Vladimir V. Riabov

    E-Print Network [OSTI]

    Riabov, Vladimir V.

    for the transition flow regime have been found: non-monotonic lift and drag of plates, strong repulsive force between side-by-side plates and cylinders, dependence of drag on torus radii ratio, and the reverse Magnus devices, and in micro-channels. Numerous results were found in the cases of plates, wedges, cones, spheres

  13. NREL Studies Wind Farm Aerodynamics to Improve Siting (Fact Sheet)

    SciTech Connect (OSTI)

    Not Available

    2012-04-01

    NREL researchers have used high-tech instruments and high-performance computing to understand atmospheric turbulence and turbine wake behavior in order to improve wind turbine design and siting within wind farms.

  14. AERODYNAMICS RESEARCH CENTER MECHANICAL AND AEROSPACE ENGINEERING DEPARTMENT

    E-Print Network [OSTI]

    Texas at Arlington, University of

    MECHANICAL AND AEROSPACE ENGINEERING DEPARTMENT IntroductionIntroduction PDEs viable for supersonic & hypersonic military and civilianPDEs viable for supersonic & hypersonic military and civilian applications.systems. PDE as afterburner in turbojets.PDE as afterburner in turbojets. PDE as combustor in Ram or Scram jets

  15. DOE's effort to reduce truck aerodynamic drag : joint experiments...

    Office of Scientific and Technical Information (OSTI)

    2004-06-01 OSTI Identifier: 957208 Report Number(s): SAND2004-3067C TRN: US201007%%510 DOE Contract Number: AC04-94AL85000 Resource Type: Conference Resource Relation:...

  16. A model for aerodynamically-valved pulse combustion

    SciTech Connect (OSTI)

    Richards, G.A. [USDOE Morgantown Energy Technology Center, WV (United States); Narayanaswami, L.L. [Embry-Riddle Aeronautical Univ., Daytona Beach, FL (United States)

    1992-04-01

    This paper presents a simulation of aerovalve pulse combustion. Starting from the conservative laws, a simplified set of governing equations that identifies crucial parameters is obtained. The combustor is assumed to be well-stirred, and modified slug flow models are applied to the flows in the inlet and exit pipes. The simulation has been used to study the influence of geometry and operational parameters on the operation of the pulse combustor.

  17. A model for aerodynamically-valved pulse combustion

    SciTech Connect (OSTI)

    Richards, G.A. (USDOE Morgantown Energy Technology Center, WV (United States)); Narayanaswami, L.L. (Embry-Riddle Aeronautical Univ., Daytona Beach, FL (United States))

    1992-01-01

    This paper presents a simulation of aerovalve pulse combustion. Starting from the conservative laws, a simplified set of governing equations that identifies crucial parameters is obtained. The combustor is assumed to be well-stirred, and modified slug flow models are applied to the flows in the inlet and exit pipes. The simulation has been used to study the influence of geometry and operational parameters on the operation of the pulse combustor.

  18. Aerodynamic Shape Design of Nozzles Using a Hybrid Optimization Method

    E-Print Network [OSTI]

    Xing, X.Q.

    A hybrid design optimization method combining the stochastic method based on simultaneous perturbation stochastic approximation (SPSA) and the deterministic method of Broydon-Fletcher-Goldfarb-Shanno (BFGS) is developed ...

  19. Structural and Aerodynamic Interaction Computational Tool for Highly Reconfigurable Wings

    E-Print Network [OSTI]

    Eisenbeis, Brian Joseph

    2011-10-21

    Morphing air vehicles enable more efficient and capable multi-role aircraft by adapting their shape to reach an ideal configuration in an ever-changing environment. Morphing capability is envisioned to have a profound impact on the future...

  20. Optimum Aerodynamic Design using the Navier--Stokes Equations

    E-Print Network [OSTI]

    Pierce, Niles A.

    Princeton, New Jersey 08544 USA and y Oxford University Computing Laboratory Numerical Analysis Group Oxford until an optimum solution is approached. Each design cycle requires the numerical solution of both the flow and the adjoint equations, leading to a computational cost roughly equal to the cost of two flow

  1. A Computational Study of the Aerodynamics and Aeroacoustics of...

    Broader source: All U.S. Department of Energy (DOE) Office Webpages (Extended Search)

    Laboratories, Albuquerque, NM, 87185-1124, USA C. Eric Lynch and Marilyn J. Smith Georgia Institute of Technology, Atlanta, Georgia, 30332-0150, USA This work...

  2. Fleet Evaluation and Factory Installation of Aerodynamic Heavy...

    Office of Scientific and Technical Information (OSTI)

    of refinement. The fleet test undertaken showed an improvement of 5.5 - 7.8% fuel economy with the devices (This does not include tire contribution). Authors: Beck, Jason ;...

  3. Multi-Resolution Simulations of Delta/Diamond Wing Aerodynamics

    E-Print Network [OSTI]

    Cooper, Jacob

    2014-08-12

    establish the key flow feature differences between round and sharp leading edge wing at different length scales of motion. Features of interest are the intensity of the vortex structure, the levels of turbulence, surface streamline patterns, and surface...

  4. First international conference in numerical and experimental aerodynamics of

    E-Print Network [OSTI]

    separation location. Jet to crossflow velocity ratios (B) of 1.5 and 3 are explored. As the jets inject into the crossflow, counter-rotating vortex pairs (CVPs) are formed enhancing the mixing of high momentum outer fluid

  5. Aerodynamic Optimization Algorithm with Integrated Geometry Parameterization and Mesh Movement

    E-Print Network [OSTI]

    Zingg, David W.

    production [2,3]. These problems may eventually be solved by alternative fuels such as hydrogen and bio-kerosene. However, when production emissions are included, these alternative fuels presently produce more green- house gases than traditional kerosene [4]. Alternative fuels must therefore be considered a long

  6. Aerodynamic Design for Swept-wing Laminar Flow

    E-Print Network [OSTI]

    Belisle, Michael Joseph

    2013-11-08

    (SARGE), a natural laminar flow and passive laminar flow control wing glove flight experiment funded by the NASA Environmentally Responsible Aviation initiative. The experiment seeks to raise the technology readiness level of the spanwise...

  7. Aerodynamic Shape Optimization of Benchmark Problems Using Jetstream

    E-Print Network [OSTI]

    Zingg, David W.

    The dual forces of growing concern over the negative impact of carbon emissions in the environment and the rise of jet fuel prices pressure aircraft manufacturers to prioritize minimizing fuel burn when American Institute of Aeronautics and Astronautics #12;the process, 72 billion gallons of jet fuel were

  8. DOE's effort to reduce truck aerodynamic drag through joint experiment...

    Office of Scientific and Technical Information (OSTI)

    Resource Relation: Conference: Proposed for presentation at the Society of Automotive Engineers; Commercial Vehicle held November 1-3, 2005 in Chicago, IL. Research Org:...

  9. In Conjunction with Applied Mathematics Institute Wind Turbine Aerodynamics: Some

    E-Print Network [OSTI]

    Yu, Xinwei

    , that developed small wind turbine technology which he started after many years teaching at the University Springer on-line journal. His book Small Wind Turbines was published by Springer in 2011. #12;

  10. Aerodynamic Models for Hurricanes III. Modeling hurricane boundary layer

    E-Print Network [OSTI]

    Leonov, Arkady I

    2008-01-01

    The third paper of the series (see previous ones in Refs.[1-2]) discusses basic physicalprocesses in the (quasi-) steady hurricane boundary layer (HBL), develops an approximate airflow model, establishes the HBL structure, and presents integral balance relations for dynamic and thermodynamic variables in HBL. Models of evaporation and condensation are developed, where the condensation is treated similarly to the slow combustion theory. A turbulent approximation for the lower sub-layer of HBL is applied to the sea-air interaction to establish the observed increase in angular momentum in the outer region of HBL.A closed set of balance relations has been obtained. Simple analytical solution of the set yields expressions for the basic dynamic variables - maximal tangential and radial velocities in hurricane, maximal vertical speed in eye wall, the affinity speed of hurricane travel, and the maximal temperature increase after condensation. Estimated values of the variables seem to be realistic. An attempt is also ...

  11. Active Aerodynamic Blade Distributed Flap Control Design Procedure

    Broader source: All U.S. Department of Energy (DOE) Office Webpages (Extended Search)

    AFDC Printable Version Share this resource Send a link to EERE: Alternative Fuels Data Center Home Page to someone by E-mail Share EERE: Alternative Fuels Data Center Home Page on Facebook Tweet about EERE: Alternative Fuels Data Center Home Page on Twitter Bookmark EERE: Alternative Fuels Data Center Homesum_a_epg0_fpd_mmcf_m.xls" ,"Available from WebQuantity ofkandz-cm11 OutreachProductswsicloudwsicloudden DocumentationAccommodationsRegister / Vol. 72, No. 39 1S1!4T op

  12. Aerodynamic and Aeroacoustic Properties of a Flatback Airfoil: An Update

    Broader source: All U.S. Department of Energy (DOE) Office Webpages (Extended Search)

    AFDC Printable Version Share this resource Send a link to EERE: Alternative Fuels Data Center Home Page to someone by E-mail Share EERE: Alternative Fuels Data Center Home Page on Facebook Tweet about EERE: Alternative Fuels Data Center Home Page on Twitter Bookmark EERE: Alternative Fuels Data Center Homesum_a_epg0_fpd_mmcf_m.xls" ,"Available from WebQuantity ofkandz-cm11 OutreachProductswsicloudwsiclouddenDVA N C E D B L O O D S TA I N P A T T E R N A NA LY S I

  13. ACARS Aerodynamic (Research Incorporated) Communication and Recording System

    Broader source: All U.S. Department of Energy (DOE) Office Webpages (Extended Search)

    AFDC Printable Version Share this resource Send a link to EERE: Alternative Fuels Data Center Home Page to someone by E-mail Share EERE: Alternative Fuels Data Center Home Page on Facebook Tweet about EERE: Alternative Fuels Data Center Home Page on Twitter Bookmark EERE: Alternative Fuels Data Center Homesum_a_epg0_fpd_mmcf_m.xls" ,"Available from WebQuantity ofkandz-cm11 Outreach HomeA Better Anode Design to Improve4AJ01) (See Energy Level79AJ01) (NotAdvanced ABSTRACTS FOR3 -ix

  14. DOE's effort to reduce truck aerodynamic drag : joint experiments and

    Office of Scientific and Technical Information (OSTI)

    AFDC Printable Version Share this resource Send a link to EERE: Alternative Fuels Data Center Home Page to someone by E-mail Share EERE: Alternative Fuels Data Center Home Page on Facebook Tweet about EERE: Alternative Fuels Data Center Home Page on Twitter Bookmark EERE: Alternative Fuels Data Center Homesum_a_epg0_fpd_mmcf_m.xls" ,"Available from WebQuantity of NaturalDukeWakefieldSulfate Reducing BacteriaConnect Collidertransfer (Journal Article) |Programs ofReport

  15. Aerodynamic Drag Reduction Apparatus For Wheeled Vehicles In Ground Effect

    Office of Scientific and Technical Information (OSTI)

    AFDC Printable Version Share this resource Send a link to EERE: Alternative Fuels Data Center Home Page to someone by E-mail Share EERE: Alternative Fuels Data Center Home Page on Facebook Tweet about EERE: Alternative Fuels Data Center Home Page on Twitter Bookmark EERE: Alternative Fuels Data Center Homesum_a_epg0_fpd_mmcf_m.xls" ,"Available from WebQuantity of NaturalDukeWakefield MunicipalTechnicalInformation4563Abuse Tolerance(Conference)Geothermal Reservoirs:Adventures on

  16. Aerodynamic Drag Reduction Apparatus For Wheeled Vehicles In Ground Effect

    Office of Scientific and Technical Information (OSTI)

    AFDC Printable Version Share this resource Send a link to EERE: Alternative Fuels Data Center Home Page to someone by E-mail Share EERE: Alternative Fuels Data Center Home Page on Facebook Tweet about EERE: Alternative Fuels Data Center Home Page on Twitter Bookmark EERE: Alternative Fuels Data Center Homesum_a_epg0_fpd_mmcf_m.xls" ,"Available from WebQuantity of NaturalDukeWakefield MunicipalTechnicalInformation4563Abuse Tolerance(Conference)Geothermal Reservoirs:Adventures

  17. Fleet Evaluation and Factory Installation of Aerodynamic Heavy Duty Truck

    Office of Scientific and Technical Information (OSTI)

    AFDC Printable Version Share this resource Send a link to EERE: Alternative Fuels Data Center Home Page to someone by E-mail Share EERE: Alternative Fuels Data Center Home Page on Facebook Tweet about EERE: Alternative Fuels Data Center Home Page on Twitter Bookmark EERE: Alternative Fuels Data Center Homesum_a_epg0_fpd_mmcf_m.xls" ,"Available from WebQuantity of NaturalDukeWakefieldSulfate Reducing(Journal Article) |production atmeasurement forces.comparisonTrailers (Technical Report)

  18. Fleet Evaluation and Factory Installation of Aerodynamic Heavy Duty Truck

    Office of Scientific and Technical Information (OSTI)

    AFDC Printable Version Share this resource Send a link to EERE: Alternative Fuels Data Center Home Page to someone by E-mail Share EERE: Alternative Fuels Data Center Home Page on Facebook Tweet about EERE: Alternative Fuels Data Center Home Page on Twitter Bookmark EERE: Alternative Fuels Data Center Homesum_a_epg0_fpd_mmcf_m.xls" ,"Available from WebQuantity of NaturalDukeWakefieldSulfate Reducing(Journal Article) |production atmeasurement forces.comparisonTrailers (Technical

  19. Integrated External Aerodynamic and Underhood Thermal Analysis for Heavy

    Office of Energy Efficiency and Renewable Energy (EERE) Indexed Site

    AFDC Printable Version Share this resource Send a link to EERE: Alternative Fuels Data Center Home Page to someone by E-mail Share EERE: Alternative Fuels Data Center Home Page on Facebook Tweet about EERE: Alternative Fuels Data Center Home Page on Twitter Bookmark EERE: Alternative Fuels Data Center Home Page on Google Bookmark EERE: Alternative Fuels Data Center Home Page on Delicious RankADVANCED MANUFACTURING OFFICE INDUSTRIAL TECHNICAL8-02 InspectionCONFERENCE ofPilot

  20. High-solids paint overspray aerosols in a spray painting booth: particle size analysis and scrubber efficiency

    SciTech Connect (OSTI)

    Chan, T.L.; D'arcy, J.B.; Schreck, R.M.

    1986-07-01

    Particle size distributions of high-solids acrylic-enamel paint overspray aerosols were determined isokinetically in a typical downdraft spray painting booth in which a 7-stage cascade impactor was used. Three different industrial paint atomizers were used, and the paint aerosols were characterized before and after a paint both scrubber. The mass median aerodynamic diameter (MMAD) of a metallic basecoat and an acrylic clearcoat paint aerosol from air-atomized spray guns ranged from 4-12 ..mu..m and was dependent on atomization pressure. When the paint booth was operated under controlled conditions simulating those in a plant, the collection efficiency of paint overspray aerosols by a paint scrubber was found to be size dependent and decreased sharply for particles smaller than 2 ..mu..m to as low as 64% for clearcoat paint particles of 0.6 ..mu..m. Improvement in the overall particulate removal efficiency can be achieved by optimizing the spray painting operations so as to produce the least amount of fine overspray paint aerosols less than 2 ..mu..m. Maintaining a higher static pressure drop across the paint both scrubber also will improve scrubber performance.

  1. 186 IEEE SIGNAL PROCESSING LETTERS, VOL. 6, NO. 7, JULY 1999 Vector Median-Rational Hybrid Filters

    E-Print Network [OSTI]

    Gabbouj, Moncef

    @cs.tut.fi). M. Gabbouj is with the Signal Processing Laboratory, Tampere University of Technology, FIN-33 101

  2. Integrating Normative Location Models into GIS: Problems and Prospects with the p-median Model (94-5)

    E-Print Network [OSTI]

    Church, Richard L.; Sorensen, Paul

    1994-01-01

    Normative Location Models into GIS: Problems and ProspectsNormative Location Models into GIS: problems and prospectsInformation Systems (GIS). This includes such normative

  3. "Block" "Spot Column" "Spot Row" ORF ID Gene Block Column Row Name ID X Y Dia. F635 Median F635 Mean F635 SD B635 Median B635 Mean B635 SD % > B635+1SD % > B635+2SD F635 % Sat. F532 Median F532 Mean F532 SD B532 Median B532 Mean B532 SD % > B532+1SD % > B

    E-Print Network [OSTI]

    Winston, Fred

    622 100 100 0 2580 2796 1174 63 89 234 100 100 0 5.257 5.315 5.223 5.619 2.874 5.004 0.873 2.394 13231

  4. Atmos. Chem. Phys., 11, 13271337, 2011 www.atmos-chem-phys.net/11/1327/2011/

    E-Print Network [OSTI]

    Meskhidze, Nicholas

    . A quantitative energy-dispersive electron probe X-ray microanalysis (ED-EPMA), called low-Z particle EPMA for fine aerosol particles (2.5 m in aerodynamic diameter). The emission of air pollutants from motor (through industrial and other human activities) and from gas-to-particle conversion (Watson, 2002). In turn

  5. SANDIA REPORT SAND791753 q Unlimited Release q UC60 Reprinted August 1982

    E-Print Network [OSTI]

    -BladedTest Data Summary 5 #12;Figure 1. DOE/Sandia17-m Wind Turbine #12;Aerodynamic WINX `TURBINEIN PERFORMANCEOF Performance of the 17-M-Diameter Darrieus Wind Turbine in the Three-Bladed Configuration: An Addendum Mark H ABSTRACT The U.S. Departmentof Energy (DOE)/Sandia17-m wind turbine has been tested in the three

  6. Experimental study of nuclear workplace aerosol samplers

    E-Print Network [OSTI]

    Parulian, Antony

    1995-01-01

    consists of an inlet-elbow, a transport line, and a EL-900 CAM prototype manufactured by EG&G. Results show that only 12% of 10 []m aerodynamic diameter (AD) aerosol particles penetrate through the complete sampling system when it is operated at flow rate...

  7. This invention relates to methods of generating NP gallium nitride (GaN) across large areas (>1 cm.sup.2) with controlled pore diameters, pore density, and porosity. Also disclosed are methods of generating novel optoelectronic devices based on porous GaN. Additionally a layer transfer scheme to separate and create free-standing crystalline GaN thin layers is disclosed that enables a new device manufacturing paradigm involving substrate recycling. Other disclosed embodiments of this invention relate to fabrication of GaN based nanocrystals and the use of NP GaN electrodes for electrolysis, water splitting, or photosynthetic process applications.

    DOE Patents [OSTI]

    Zhang, Yu; Sun, Qian; Han, Jung

    2015-12-08

    This invention relates to methods of generating NP gallium nitride (GaN) across large areas (>1 cm.sup.2) with controlled pore diameters, pore density, and porosity. Also disclosed are methods of generating novel optoelectronic devices based on porous GaN. Additionally a layer transfer scheme to separate and create free-standing crystalline GaN thin layers is disclosed that enables a new device manufacturing paradigm involving substrate recycling. Other disclosed embodiments of this invention relate to fabrication of GaN based nanocrystals and the use of NP GaN electrodes for electrolysis, water splitting, or photosynthetic process applications.

  8. Chemical distribution in high-solids paint overspray aerosols

    SciTech Connect (OSTI)

    D'Arcy, J.B.; Chan, T.L. )

    1990-03-01

    The chemical composition of high-solids basecoat paint overspray aerosols was determined as a function of particle size. Detailed information on the chemical composition of the overspray aerosols is important in health hazard evaluation since the composition and distribution within the airborne particles may differ significantly from the bulk paint material. This study was conducted in a typical down-draft paint booth equipped with air-atomized spray painting equipment. A fixed paint target was used to simulate typical overspray generation conditions and the aerosols were collected isokinetically with a seven-stage cascade impactor for size-fractionated analysis. The overspray aerosol from six paints consisted of organic paint binders with varying amounts of inorganic species as pigments or luster enhancers. These overspray aerosols had mass median aerodynamic diameters (MMAD) ranging from 2.9 to 9.7 microns. The size-fractionated paint samples collected on the impaction stages were analyzed by energy dispersive X-ray spectrometry on a scanning electron microscope (SEM-EDXRS) to identify the metallic elements. Atomic absorption spectrometry was used to determine the mass distribution of aluminum and iron as indicators of nonuniform distribution. Three of the aerosols containing aluminum were found to have bimodal distributions with most aluminum distributions having cumulative MMADs larger than the total aerosol. Iron in the aerosols was bimodal for three of the paints with all samples having an overall iron MMAD less than or equal to the overspray aerosol MMAD. Analysis using ultraviolet spectrometry revealed that the organic compounds present in the size-fractionated particulate samples consisted of a single, polydispersed mode with an MMAD similar to that of the total overspray aerosol.

  9. Measurements of trace element concentration profiles across the diameter of human hair with micro-pixe

    SciTech Connect (OSTI)

    Bos, A.J.J.; C.C.A.H.v.d. Stap.; Lenglet, W.J.M.; Valkovic, V.; Vis, R.D.

    1983-04-01

    Trace element distributions across single human hairs using a proton microbeam has been measured to study the origin of these elements in hair. A new way of concentration assignment for micro PIXE making use of both the Proton Induced characteristic X-rays and the Rutherford Backscattered protons is reported.

  10. UBC Social Ecological Economic Development Studies (SEEDS) Student Report Marketing Strategy for Small Diameter Douglas Fir

    E-Print Network [OSTI]

    Tables $900.00 per table 48.7% 5.0% 124$ Total 100% 31$ PRICING INFORMATION Net Profit per Log Selling Price #12;iii TABLE OF CONTENTS ABSTRACT and price potential. The product line included a flooring system, acoustic-ceiling panels, RTA tabletops

  11. tures, ~200 m in diameter, surrounding a central blood vessel. Compact bone, solid to

    E-Print Network [OSTI]

    to that of fiber-reinforced plastics. However, they consist of a compos- ite in which fibers and matrix mollusk shells. The crossed-lamel- lar structure consists almost entirely of cal- cium carbonate, with a layer of organic material surrounding the fibers (7). Furthermore, the magnesium content of the calcite

  12. Polyaniline nanofiber based surface acoustic wave gas sensors - Effect of nanofiber diameter on H-2 response

    E-Print Network [OSTI]

    Sadek, A Z; Baker, Christina Opimo; Powell, D A; Wlodarski, W; Kaner, R B; Kalantar-zadeh, K

    2007-01-01

    Nano?ber Based Surface Acoustic Wave Gas SensorsEffect ofYX LiNbO 3 sur- face-acoustic-wave transducers. The sensorsrapidly mixed, surface acoustic wave (SAW). I. I NTRODUCTION

  13. A Comprehensive Strategy for Value-Driven Utilisation of Douglas-fir Small Diameter Roundwood

    E-Print Network [OSTI]

    ------------------------------------------------------------------------------------------- 8 Areas of Growth ------------------------------------------------------------------------------------------------------16 Technology

  14. Polyaniline nanofiber based surface acoustic wave gas sensors - Effect of nanofiber diameter on H-2 response

    E-Print Network [OSTI]

    Sadek, A Z; Baker, Christina Opimo; Powell, D A; Wlodarski, W; Kaner, R B; Kalantar-zadeh, K

    2007-01-01

    acoustic wave due to piezoelectric effects. The center frequency of a SAW device is given by the equation

  15. Forced-convection surface-boiling heat transfer and burnout in tubes of small diameters

    E-Print Network [OSTI]

    Bergles A. E.

    1962-01-01

    A basic heat-transfer apparatus was designed and constructed for the study of forced-convection boiling in small channels. The various regions of forced-convection surface boiling were studied experimentally and analytically. ...

  16. The role of apolipoprotein VLDL-II in regulating the diameter of VLDLy

    E-Print Network [OSTI]

    Wallowitz, Mikhael L

    2003-01-01

    The physiological function of each class of lipoproteins is dictated in part by the structural biology of the lipoprotein particle. Proteins embedded in the superficial phospholipid monolayer (apolipoproteins) facilitate the receptor mediated...

  17. BRANCH-BASED MODEL FOR THE DIAMETERS OF THE PULMONARY AIRWAYS...

    Office of Scientific and Technical Information (OSTI)

    ; Polissar, Nayak ; Einstein, Daniel R. ; Glenny, Robb W. ; Minard, Kevin R. ; Carson, James P. ; Jiao, Xiangmin ; Jacob, Rick E. ; Cox, Timothy C. ; Postlewait, Ed ; Corley,...

  18. SEALING LARGE-DIAMETER CAST-IRON PIPE JOINTS UNDER LIVE CONDITIONS

    SciTech Connect (OSTI)

    Kiran M. Kothari; Gerard T. Pittard

    2005-07-01

    Utilities in the U.S. operate over 75,000 km (47,000 miles) of old cast-iron pipes for gas distribution. Bell-and-spigot joints that connect pipe sections together tend to leak as these pipes age. Current repair practices are costly and highly disruptive. The objective of this program is to design, test and commercialize a robotic system capable of sealing multiple castiron bell and spigot joints from a single pipe entry point. The proposed system will perform repairs with the pipe in service by traveling through the pipe, cleaning each joint surface, and installing a stainless-steel sleeve lined with an epoxy-impregnated felt across the joint. This approach will save considerable time and labor, minimize excavation, avoid traffic disruption, and eliminate any requirement to interrupt service to customers (which would result in enormous expense to utilities). Technical challenges include: (1) repair sleeves must compensate for diametric variation and eccentricity of old cast-iron pipes; (2) the assembly must travel long distances through pipes containing debris; (3) the pipe wall must be effectively cleaned in the immediate area of the joint to assure good bonding of the sleeve; and (4) an innovative bolt-on entry fitting is required to conduct safe repair operations on live mains.

  19. Non-intrusive ultrasonic liquid-in-line detector for small diameter tubes. [Patent application

    DOE Patents [OSTI]

    Piper, T.C.

    1980-09-24

    An arrangement for detecting liquids in a line, using non-intrusive ultrasonic techniques is disclosed. In this arrangement, four piezoelectric crystals are arranged in pairs about a 0.078 inch o.d. pipe. An ultrasonic tone burst is transmitted along the pipe, between crystal pairs, and the amplitude of the received tone burst indicates the absence/presence of liquid in the pipe.

  20. SELECTED PROPERTIES OF WOOD STRAND AND ORIENTED STRANDBOARD FROM SMALL-DIAMETER SOUTHERN PINE TREES1

    E-Print Network [OSTI]

    , and bending strength and modulus varied little in the parallel direction and slightly decreased with increase of temperature in the range of 25 to 200C. Small loss modulus (E ) peaks were observed over and paper industry and restricted logging on fed- eral forest land, there is an overstocking of small

  1. Laser amplifier based on a neodymium glass rod 150 mm in diameter

    SciTech Connect (OSTI)

    Shaykin, A A; Fokin, A P; Soloviev, A A; Kuzmin, A A; Shaikin, I A; Burdonov, K F; Khazanov, E A [Institute of Applied Physics, Russian Academy of Sciences, Nizhnii Novgorod (Russian Federation); Charukhchev, A V [Public Limited Company "Scientific research Institute for Optoelectronic Instrument Engineering", Leningrad region (Russian Federation)

    2014-05-30

    A unique large-aperture neodymium glass rod amplifier is experimentally studied. The small-signal gain distribution is measured at different pump energies. The aperture-averaged gain is found to be 2.3. The stored energy (500 J), the maximum possible pump pulse repetition rate, and the depolarisation in a single pulse and in a series of pulses with a repetition rate of one pulse per five minutes are calculated based on the investigations performed. It is shown that the use of this amplifier at the exit of the existing laser can increase the output pulse energy from 300 to 600 J. (lasers)

  2. RESEARCH Open Access Estimation of optic nerve sheath diameter on an

    E-Print Network [OSTI]

    Boyer, Edmond

    , mortality in the United States was reportedly higher (18.4 per 100,000) [1]. Post- TBI disability is a major) measured on the initial brain computed tomography (CT) scan for intensive care unit (ICU) mortality is independently associated with ICU mortality rate (when 7.3 mm) in severe TBI patients. Introduction Severe

  3. Development length of three-eights inch diameter, seven-wire concrete prestressing cable

    E-Print Network [OSTI]

    George, Jimmy Donnell

    1968-01-01

    in this f LC3d, but none of the findin!&;s have produ(ed. sny conclusive Ie- sults. Xn tile early days of prc-tensioned. pl estre, ' sed con- crete, re. , eaI chere thou~~ht that, 'ihe amount of tension placed in s, pxestressed stI and vvas a factor...brlt7rttt3. j t . I3 tO t;iO G RttGli, i't &lO J. . t Or~6 Ct f ptAl' Ct r'1 f7rC fX t ', . ''Ol I t Of '(''1C 7' . Cr7411 ':I ', . t'i Ltr 7 OF UJ' r. : C 'Cx'O0 Of Ji!raiy Troop l. l. Coors e Ao'u&o s'eel e. e I. o, ' c. vl e 8! i(T o oYl %co...

  4. 2005 Proc. Annu. Conf. SEAFWA Relationship of Oak Seedling Height and Diameter

    E-Print Network [OSTI]

    Gray, Matthew

    and other wetlands was authorized by the Clean Water Act of 1977 (Mitsch and Gosselink 2000). In addition, the Swamp- buster Provision of the Food Security Act of 1985 disqualified farmers from receiv- ing federal and improve water quality by naturally filtering sediments and contaminants from runoff (Gosselink and Lee

  5. Modeling Ozone Removal to Indoor Materials, Including the Effects of Porosity, Pore Diameter, and Thickness

    E-Print Network [OSTI]

    Gall, Elliott T; Siegel, Jeffrey A; Corsi, Richard L

    2015-01-01

    of healthy young volunteers to ozone causes cardiovasculareffects of five common ozone-initiated terpene reactiondecay rates, and removal of ozone and their relation to

  6. Strain-Based Design Methodology of Large Diameter Grade X80 Linepipe

    SciTech Connect (OSTI)

    Lower, Mark D.

    2014-04-01

    Continuous growth in energy demand is driving oil and natural gas production to areas that are often located far from major markets where the terrain is prone to earthquakes, landslides, and other types of ground motion. Transmission pipelines that cross this type of terrain can experience large longitudinal strains and plastic circumferential elongation as the pipeline experiences alignment changes resulting from differential ground movement. Such displacements can potentially impact pipeline safety by adversely affecting structural capacity and leak tight integrity of the linepipe steel. Planning for new long-distance transmission pipelines usually involves consideration of higher strength linepipe steels because their use allows pipeline operators to reduce the overall cost of pipeline construction and increase pipeline throughput by increasing the operating pressure. The design trend for new pipelines in areas prone to ground movement has evolved over the last 10 years from a stress-based design approach to a strain-based design (SBD) approach to further realize the cost benefits from using higher strength linepipe steels. This report presents an overview of SBD for pipelines subjected to large longitudinal strain and high internal pressure with emphasis on the tensile strain capacity of high-strength microalloyed linepipe steel. The technical basis for this report involved engineering analysis and examination of the mechanical behavior of Grade X80 linepipe steel in both the longitudinal and circumferential directions. Testing was conducted to assess effects on material processing including as-rolled, expanded, and heat treatment processing intended to simulate coating application. Elastic-plastic and low-cycle fatigue analyses were also performed with varying internal pressures. Proposed SBD models discussed in this report are based on classical plasticity theory and account for material anisotropy, triaxial strain, and microstructural damage effects developed from test data. The results are intended to enhance SBD and analysis methods for producing safe and cost effective pipelines capable of accommodating large plastic strains in seismically active arctic areas.

  7. An improved analytical detector response function model for multilayer small-diameter PET scanners

    E-Print Network [OSTI]

    Strul, D; Slates, R B; Dahlbom, M; Cherry, Simon R; Marsden, P K

    2003-01-01

    of microPET: a high-resolution lutetium oxyorthosilicate PETlayer, scanners employing lutetium oxyorthosilicate (LSO)

  8. diameter. During skimmed milk MF the fouling, mainly due to a deposit of casein

    E-Print Network [OSTI]

    Paris-Sud XI, Universit de

    of casein micelles from soluble proteins of skimmed milk can be achieved by crossflow micro- filtration, MF, using a 0.1 m mean pore Original article Critical stability conditions in skimmed milk crossflow Abstract -- There exists a critical ratio (convection towards the membrane/erosion) in crossflow micro

  9. Modeling Ozone Removal to Indoor Materials, Including the Effects of Porosity, Pore Diameter, and Thickness

    E-Print Network [OSTI]

    Gall, Elliott T; Siegel, Jeffrey A; Corsi, Richard L

    2015-01-01

    C. Ozone deposition velocities, reaction probabilities andreaction phenomena described by a single parameter, the ozone deposition velocity,velocity, v t (m h ?1 ), a characteristic of the ?uid mechanics of a space, and the reaction

  10. a 3.37 mm length b 3.32 mm diameter

    E-Print Network [OSTI]

    Marc, Robert E.

    5.2 ml retinal subtense 300 m/deg retinal arc 51 mm retinal area* 1024 184 mm2 total.3 l retinal subtense 31 m/deg retinal arc 4.9 mm retinal area 15.6 mm2 cone:rod ratio 0/deg retinal arc 10.6 mm retinal area 52 mm2 cone:rod ratio mean cone density* mm-2 mean rod

  11. Pulling of 3 mm diameter AlSb rods by micro-pulling down method

    E-Print Network [OSTI]

    Bourret-Courchesne Ph.D., Edith

    2009-01-01

    Sb) and AlSb crystal zirconia were expected as crucibles,crucible shape with zirconia. Page 3/10 Fig 1 : vitreous

  12. Measurement of emission diameter as a function of time on foam z- pinch plasmas

    SciTech Connect (OSTI)

    Lazier, S.E.; Barber, T.L. [Ktech Corp., Albuquerque, NM (United States); Derzon, M.S.; Kellogg, J.W.

    1996-05-14

    We have developed a streaked imaging capability to make time-resolved measurements of the emission size for low density foam z-pinches. By lens coupling visible emission from the z-pinch target to an array of fiber optics we obtained the emission profile in the visible as a function of time with radial resolution of 300 {mu}m. To measure the emission at temperatures greater than {approx}40 eV the source was slit-imaged or pin-hole imaged onto an x-ray filtered scintillator. Non-uniformities in both visible and x-ray emission were observed. We describe the diagnostics, the image unfold process, and results from the instrument for both visible and x-ray measurements.

  13. PHYSICAL REVIEW A 86, 013804 (2012) Diameter-bandwidth product limitation of isolated-object cloaking

    E-Print Network [OSTI]

    2012-01-01

    , Massachusetts 02139, USA 4 WiTricity Corporation, Watertown, Massachusetts 02472, USA (Received 20 March 2012

  14. In-line inspection of large diameter pipelines using enhanced collapsible pigs

    SciTech Connect (OSTI)

    Pikas, J.L.

    1996-08-01

    In-line inspection tools, smart pigs, are devices that detect magnetic irregularities or anomalies in the wall of the pipe that includes corrosion, gouges, and material defects that exhibit metal loss. However, they do not normally detect stress corrosion cracking (SCC), hydrogen embrittlement, hard spots, certain types of horizontal defects, and anomalies on or near the girth weld. Dents if significant, casings, and foreign metallic objects if touching the pipe may also be detected qualitatively. Also, features such as welds, valves, taps, flanges, test station plates, and other appurtenances can be identified. Case histories and field findings using the newly developed 30 inch x 24 inch and 36 inch x 30 inch collapsible smart pigs will be discussed. In addition, the results of the first generation smart pigs with enhancements consisting of hardware developments, new field logs, and software will be presented.

  15. Correlation between catalyst particle and single-walled carbon nanotube diameters

    E-Print Network [OSTI]

    Machinery and Design, Seoul National University, Seoul 151-742, South Korea c VTT Processes, Aerosol

  16. Calibration of a Neutron Hydroprobe for Moisture Measurements in Small-Diameter Steel-Cased Boreholes

    SciTech Connect (OSTI)

    Ward, Anderson L.; Wittman, Richard S.

    2009-08-01

    Computation of soil moisture content from thermalized neutron counts for the T-Farm Interim cover requires a calibration relationship but none exists for 2-in tubes. A number of calibration options are available for the neutron probe, including vendor calibration, field calibration, but none of these methods were deemed appropriate for the configuration of interest. The objective of this work was to develop a calibration relation for converting neutron counts measured in 2-in access tubes to soil water content. The calibration method chosen for this study was a computational approach using the Monte Carlo N-Particle Transport Code (MCNP). Model calibration was performed using field measurements in the Hanford calibration models with 6-in access tubes, in air and in the probe shield. The bet-fit model relating known water content to measured neutron counts was an exponential model that was essentially equivalent to that currently being used for 6-in steel cased wells. The MCNP simulations successfully predicted the neutron count rate for the neutron shield and the three calibration models for which data were collected in the field. However, predictions for air were about 65% lower than the measured counts . This discrepancy can be attributed to uncertainties in the configuration used for the air measurements. MCNP-simulated counts for the physical models were essentially equal to the measured counts with values. Accurate prediction of the response in 6-in casings in the three calibration models was motivation to predict the response in 2-in access tubes. Simulations were performed for six of the seven calibration models as well as 4 virtual models with the entire set covering a moisture range of 0 to 40%. Predicted counts for the calibration models with 2-in access tubes were 40 to 50% higher than in the 6-inch tubes. Predicted counts for water were about 60% higher in the 2-in tube than in the 6-in tube. The discrepancy between the 2-in and 6-in tube can be attributed to the smaller air gap between the probe and the 2-in access tube. The best-fit model relating volumetric water content to count ratio (CR) is of the form e^A x CR^B with A=0.3596 0.0216 and B=0.4629 0.0629 and r^2= 0.9998. It is recommended that the calibration function based on the count ratio, rather than raw counts, be used to avoid the effects of electronic noise in the probe that may arise due to the conditions at the time of measurement. These results suggest that the MCNP code can be used to extend calibrations for the neutron probe to different conditions including access tube size as well as composition without the need to construct additional physical models.

  17. Economic and Performance Benefits Resulting From the Use of Large Diameter

    Open Energy Info (EERE)

    AFDC Printable Version Share this resource Send a link to EERE: Alternative Fuels Data Center Home Page to someone by E-mail Share EERE: Alternative Fuels Data Center Home Page on Facebook Tweet about EERE: Alternative Fuels Data Center Home Page on Twitter Bookmark EERE: Alternative Fuels Data Center Home Page on Google Bookmark EERE: Alternative Fuels Data Center Home Page on QA:QA J-E-1 SECTION J APPENDIX ECoopButtePower VenturesInformation9)askDoubleEERESodaEconomic Values Jump to:Fans

  18. BRANCH-BASED MODEL FOR THE DIAMETERS OF THE PULMONARY AIRWAYS: ACCOUNTING

    Office of Scientific and Technical Information (OSTI)

    AFDC Printable Version Share this resource Send a link to EERE: Alternative Fuels Data Center Home Page to someone by E-mail Share EERE: Alternative Fuels Data Center Home Page on Facebook Tweet about EERE: Alternative Fuels Data Center Home Page on Twitter Bookmark EERE: Alternative Fuels Data Center Homesum_a_epg0_fpd_mmcf_m.xls" ,"Available from WebQuantity of NaturalDukeWakefieldSulfate Reducing Bacteria (Technical Report) | SciTech ConnectPatent:(n,3n)B-FactoriesBSciTechFOR

  19. A key feature of locomotor anatomy in fishes is the dorsal fin, which is one of three median fins, together with the anal

    E-Print Network [OSTI]

    Lauder, George V.

    of fishes has been the subject of limited experimental study compared with other propulsor systems specialized swimming modes in which the dorsal fin is employed as a key propulsor. Particular attention has-vortical (drag) wake is hypothesized as a mechanism for enhancing tail thrust. This study provides the first

  20. Correlation between Median Household Income and LEED Sustainable Site Criteria for Public Transportation Access and a Regression Model Predicting Appraised Unit Value of Unimproved Parcels in Houston, Texas

    E-Print Network [OSTI]

    Ji, Qundi

    2010-07-14

    The Leadership in Energy and Environmental Design (LEED) Green Building Rating System provides third-party verification for environmentally sustainable construction. LEED certified buildings often provide healthier work ...

  1. EROSION PREDICTION NEAR A STAGNATION POINT RESULTING FROM AERODYNAMICALLY ENTRAINED SOLID PARTICLES

    E-Print Network [OSTI]

    Laitone, J. A.

    2011-01-01

    geothermal cnnversion, and coal gasification are three areasthe environment of a coal gasification system. Inside the

  2. Numerical computation of aerodynamic sensitivity coefficients in the transonic and supersonic regimes

    E-Print Network [OSTI]

    Elbanna, Hesham Mahmoud

    1988-01-01

    Airfoil, Me 0. 2, e 1 33 7 Sensitivity of Pressure to Maximum Camber, P1406 Airfoil, Me - 0. 2, c - 1 35 8 Sensitivity of Pressure to Location of Maximum Camber, P1406 Airfoil, Me 0. 2, a 1 9 Pressure Distribution, 36 NACA 1406 Airfoil, Me 0. 2, a 1... features that suit the 10 problem, mainly the concise description of the airfoil surfaces in terms of several geometric design variables. The expressions are as follows For parabolic-arc sections C(2Lx-x )/L 2 2 + 2Tx(l-x), x & L yu s 2 1 C[(1-2L)+2...

  3. Senior Undergraduate Student Ph.D., Associate Professor, Director of Aerodynamics and CFD Lab

    E-Print Network [OSTI]

    Zha, Gecheng

    configurations. The subsonic configuration would have a high aspect ratio and a low sweep. The aircraft would as the subsonic mode allows the aircraft to be operated on conventional runways. This paper examines some-equilibrium flow6,7 . The chemical reactions in the flow can have corrosive effects on the surface of the vehicle

  4. Aerodynamic focusing of high-density aerosols D.E. Ruiz a,n

    E-Print Network [OSTI]

    be modeled by a simple drag force within a prescribed background flowing gas. The particle-to-gas feedback to study the properties of high-density aerosol focusing for 1 m silica spheres. Preliminary results

  5. Vehicle Technologies Office Merit Review 2014: Aerodynamic Lightweight Cab Structure Components

    Broader source: Energy.gov [DOE]

    Presentation given by Pacific Northwest National Laboratory at 2014 DOE Hydrogen and Fuel Cells Program and Vehicle Technologies Office Annual Merit Review and Peer Evaluation Meeting about...

  6. The role of the aerodynamic modifications of the shapes of tall buildings

    E-Print Network [OSTI]

    Lee, Jooeun, S.M. Massachusetts Institute of Technology

    2011-01-01

    With the advances in technology, recent tall building design has undergone a shift to the free-style geometric forms in the exuberant and liberal atmosphere. As a height of the building increases, it is more susceptible ...

  7. Inertial and Aerodynamic Tail Steering of a Meso-scale Legged Robot

    E-Print Network [OSTI]

    Kohut, Nicholas Jospeh

    2013-01-01

    the ground. For early designs, high gear ratios were used toPowertrain Design Choosing the correct gear ratio for thegear, making for a more compact design. . . . . . . . . . . . . . . . . . .

  8. Development of an aerodynamic/RCS framework for the preliminary design of a hypersonic aircraft

    E-Print Network [OSTI]

    Dicara, Daniel L

    2006-01-01

    The design of hypersonic airbreathing aircraft pushes the envelope of current state-ofthe-art aerospace propulsion and materials technology. Therefore, these aircraft are highly integrated to produce adequate thrust, reduce ...

  9. Discontinuous Galerkin Methods for Computational Aerodynamics 3D Adaptive Flow Simulation with the DLR PADGE Code

    E-Print Network [OSTI]

    Hartmann, Ralf

    with the DLR PADGE Code R. Hartmann, J. Held, T. Leicht , F. Prill Deutsches Zentrum für Luft- und Raumfahrt Corresponding author Email addresses: ? Ð º ??? ?? Ð?º (R. Hartmann), ? ?º Ð Ð?º (J. Held), ?? ?ºÐ ? Ð?º (T

  10. APPLICATION OF A SYMMETRIC TOTAL VARIATION DIMINISHING SCHEME TO AERODYNAMICS OF ROTORS

    E-Print Network [OSTI]

    and present members of CFD lab for their warm friendship and support during my years in the lab. I am thanks to the former and present members of our CFD Lab: Saeid Niazi, Alex Stein, Mehmet Sahin, Guanpeng Benjanirat, and Sujeet Phanse. I would also like to thank my friends and colleagues in the Combustion Lab

  11. Aerodynamic Models for Hurricanes IV. On the hurricane genesis and maturing

    E-Print Network [OSTI]

    Leonov, Arkady I

    2008-01-01

    This, fourth paper of the series (see previous papers in Refs.[1-3]) derives approximate equations for future numerical studies of initial evolution of hurricanes, develops new analytical models of hurricane genesis and maturing, and presents simple results, which seems to be in accord with observations. Several remarks on tornados are also made at the end of the paper.

  12. Evaluation of propulsor aerodynamic performance for powered aircraft wind tunnel experiments

    E-Print Network [OSTI]

    Siu, Nina M

    2015-01-01

    This thesis describes a methodology to convert electrical power measurements to propulsor mechanical ow power for a 1:11-scale, powered wind tunnel model of an advanced civil aircraft utilizing boundary layer ingestion ...

  13. Aeolian sediment transport pathways and aerodynamics at troughs Mary C. Bourke1

    E-Print Network [OSTI]

    Bourke, Mary C.

    margin. This suggests that the threshold wind speed necessary for sand mobilization on Mars will be more; accepted 2 April 2004; published 13 July 2004. [1] Interaction between wind regimes and topography can give. These include wind streaks, falling dunes, ``lateral'' dunes, barchan dunes, linear dunes, transverse ridges

  14. LOVEL: a low-velocity aerodynamic heating code for flat-plates, wedges, and cones

    SciTech Connect (OSTI)

    Thornton, A.L.

    1981-12-01

    The LOVEL computer program calculates the boundary-layer edge conditions for subsonic and supersonic flow over flat-plate, wedge, and cone geometries for freestream Mach conditions (M/sub infinity/ < 3. Cold-wall heat-transfer calculations use reference temperature correlations based on boundary-layer edge Mach number to compute fluid properties. The first part of this report describes the theory used in the computation of the cold-wall heat-transfer rates; the second part describes in detail the input/output format for the LOVEL computer program. Outputs include freestream conditions, boundary-layer edge conditions, cold-wall heat-transfer rates, plots of heating rates, and punched-card output for use in ablation and in-depth transient heat-conduction computer codes.

  15. DOEs Effort to Reduce Truck Aerodynamic Drag through Joint...

    Office of Environmental Management (EM)

    Drag through Joint Experiments and Computations 2010 DOE Vehicle Technologies and Hydrogen Programs Annual Merit Review and Peer Evaluation Meeting, June 7-11, 2010 --...

  16. Aerodynamic effects in ink-jet printing on a moving web

    E-Print Network [OSTI]

    Hsiao, W.-K.; Hoath, S. D.; Martin, G. D.; Hutchings, I. M.

    2012-01-01

    , they normally fall within the splats formed by the deposited main drops, and hence have minimal impact on print quality. Figure 4 Deflections of the main drops, ligaments, and satellites as a function of substrate speed. Interaction... ] Tillmark, N. and Alfredsson, P.H., Experiments on transition in plane Couette flow, J. Fluid Mech. (1992), 235, 89-102. [3] Link, N., Lampert, S., Gurka, R., Liberzon, A., Hetsroni, G., and Semiat, R., Ink drop motion in wide-format printers II. Airflow...

  17. High-fidelity Aerodynamic Shape Optimization of Unconventional Aircraft through Axial Deformation

    E-Print Network [OSTI]

    Zingg, David W.

    to establish feasibility in various techno- logical and market scenarios.1719 However, while the assessment, to the design variables are calculated analytically through the discrete-adjoint method. Results point become, if it is not already, the main driving factor affecting the design of future aircraft.1

  18. 88--MarMar--0707 11AERODYNAMIC RESEARCH CENTER MECHANICAL AND AEROSPACE ENGINEERING DEPARTMENT

    E-Print Network [OSTI]

    Texas at Arlington, University of

    Development of a Compact Liquid Fueled Pulsed Detonation Engine with Pre-detonator Acknowledgements Area Change NozzleSmooth Area Change Nozzle Main CombustorMain Combustor Fuel and Gas Injection Valves Engineering, The University of Texas at Arlington, Arlington, TX, 1995. Burge, Karl Ramon, "Pulse Detonation

  19. Two-Level Free-Form Deformation for High-Fidelity Aerodynamic Shape Optimization

    E-Print Network [OSTI]

    Zingg, David W.

    awakened global awareness.1 Its disastrous impacts on the environ- ment have long been linked to oil, whose aimed at uncovering yet unknown unconventional configurations, a more flexible parameterization

  20. Aerodynamic Loads on Tall Buildings: Interactive Database Yin Zhou. M.ASCE1

    E-Print Network [OSTI]

    Kareem, Ahsan

    for possible inclusion as a design guide in the next generation of codes and standards. DOI: 10.1061/ ASCE 0733 tools in commercial design practice. However, considering the cost and lead time needed for wind tunnel.M.ASCE2 ; and Ahsan Kareem, M.ASCE3 Abstract: Under the action of wind, tall buildings oscillate

  1. Inertial and Aerodynamic Tail Steering of a Meso-scale Legged Robot

    E-Print Network [OSTI]

    Kohut, Nicholas Jospeh

    2013-01-01

    Legged Robot Maneuverability 2.1 Background . . . . .iii Robot in Free4.19 Robot body position versus time for a maximum effort

  2. New Aerodynamics Simulations Provide Better Understanding of Wind Plant Underperformance and Loading (Fact Sheet)

    SciTech Connect (OSTI)

    Not Available

    2011-02-01

    Researchers at the National Renewable Energy Laboratory (NREL) develop a high-fidelity large-eddy simulation model designed to predict the performance of large wind plants with a higher degree of accuracy than current models.

  3. Silicon micromachined sensors and sensor arrays for shear-stress measurements in aerodynamic flows

    E-Print Network [OSTI]

    Padmanabhan, Aravind

    In this thesis we report on a new micromachined floating-element shear-stress sensor for turbulent boundary layer research. Applications in low shear-stress environments such as turbulent boundary layers require extremely ...

  4. 99--MarMar--0707 11AERODYNAMIC RESEARCH CENTER MECHANICAL AND AEROSPACE ENGINEERING DEPARTMENT

    E-Print Network [OSTI]

    Texas at Arlington, University of

    system Bellini, R., and Lu, F.K., "Exergy Analysis of a Pulse Detonation Power Device", Proceedings and Thermodynamic Cycle Analysis of Air Breathing Pulse Detonation Engines", Journal of Propulsion and Power, Vol

  5. Combined Individual Pitch Control and Active Aerodynamic Load Controller Investigation for the

    E-Print Network [OSTI]

    Sandia National Laboratories P.O. Box 5800, Albuquerque, NM 87185 This paper investigates the combined uses trailing edge flap devices to reduce fatigue loads or bending moments. This work is motivated angles and rates, blade flapwise root moments, blade flapwise tip deflections, and flap bending moment

  6. DOEs Effort to Reduce Truck Aerodynamic Drag through Joint Experiments

    Broader source: Energy.gov [DOE]

    Presentation from the U.S. DOE Office of Vehicle Technologies "Mega" Merit Review 2008 on February 25, 2008 in Bethesda, Maryland.

  7. Active Aerodynamic Blade Distributed Flap Control Design Procedure for Load Reduction on the UpWind

    E-Print Network [OSTI]

    vector vmax maximum sensor output vector Technical Staff, Energy Systems Analysis/Wind and Water Power 5MW Wind Turbine David G. Wilson , Brian R. Resor , Dale E. Berg Sandia National Laboratories, P that is employed for distributed control system design for large wind turbine load reduction applications

  8. Boundary-Layer Transition Effects on Aerodynamic Characteristics of AGARD-B Model

    E-Print Network [OSTI]

    Liu, Feng

    of airplanes or airplane components, it is often desirable to simulate a flow that in most respects behaves is an ogive-cylinder with a delta wing designed for calibration of supersonic and transonic wind tunnels

  9. Aerodynamically Optimal Regional Aircraft Concepts: Conventional and Blended Wing-Body Designs

    E-Print Network [OSTI]

    Zingg, David W.

    prices and concern about both the exhaustion of fossil fuels and their contribution to climate change. Both the conventional and blended wing-body regional jets are optimized for a 500nmi mission at Mach 0, the need for more fuel efficient aircraft is becoming more pronounced for both economic and environmental

  10. The effects of heat transfer on the aerodynamic characteristics of a hot wing

    E-Print Network [OSTI]

    Macha, John Michael

    1972-01-01

    Pm. !13th the approximate temperatur. e profile, the i nteorai:ion of ti e n omentura ec!Qa r'. !0"3 '! s Pedi!cec to a fol", Peq'. ll Yi t!g Qnlp the llifo qu, dratures x T 1 0 0 (x) = exp (2 f (-. ?. ? e 2 - -, - LI, + IiJ ? d, , l 'I " ' ii 'Il...OO'(l. ". i'li: v Hsl&. "C l EO I ST I CS OF O IIOT The !&fleet?oF Peat Tf an" fef on tha ', cr odyl&an!le Charac. Ori . tie? c?f e Hot I?fi 1;. !II v 1?3 j2) John i". icha 'I uaciarf, B. . '&. . Texa ?s!1 Univers! t!; Di rerted by: inr. L), vi d J. !'Ioi...

  11. Inertial and Aerodynamic Tail Steering of a Meso-scale Legged Robot

    E-Print Network [OSTI]

    Kohut, Nicholas Jospeh

    2013-01-01

    autonomous 2.4g crawling hexapod robot. In IEEE Int. Conf.dynamics of turning in hexapods. J Exp Biol, 202(12):1603Schmitz. Hector, a new hexapod robot platform with increased

  12. Inertial and Aerodynamic Tail Steering of a Meso-scale Legged Robot

    E-Print Network [OSTI]

    Kohut, Nicholas Jospeh

    2013-01-01

    In International Symposium on Robotics, volume 30, OctoberIn IEEE Int. Conf. on Robotics and Automation, May 2013.In IEEE Int. Conf. on Robotics and Automation, Pasadena, CA,

  13. A high-order discontinuous Galerkin multigrid solver for aerodynamic applications

    E-Print Network [OSTI]

    Fidkowski, Krzysztof J., 1981-

    2004-01-01

    Results are presented from the development of a high-order discontinuous Galerkin finite element solver using p-multigrid with line Jacobi smoothing. The line smoothing algorithm is presented for unstructured meshes, and ...

  14. Two-Level Free-Form Deformation for High-Fidelity Aerodynamic Shape Optimization

    E-Print Network [OSTI]

    Zingg, David W.

    awakened global awareness.1 Its disastrous impacts on the environ- ment have long been linked to oil, whose diminishing world reserves have led to a substantial rise in fuel prices. As far as the aviation industry of incorporating an high-fidelity finite-element structural solver in the near future. Historically, shape control

  15. Strategies for mitigating wind-induced motion in tall buildings through aerodynamic and damping modifications

    E-Print Network [OSTI]

    Nnamani, Nnabuihe

    2012-01-01

    The advent of modern structural systems, spurred by advances in construction methodology and high strength materials, has driven the height of modern skyscrapers beyond what was once deemed possible. Although science and ...

  16. Code Thrust 1400 Aeronautical/Astronautical Engineering (including Aerodynamics, Aerospace Engineering, and Space Technology)

    E-Print Network [OSTI]

    Alabama in Huntsville, University of

    , Polymer, and Wood Science) 1403 Civil Engineering (including Architectural, Architecture, Environmental, Physical Chemistry, Polymer Science, excluding Biochemistry) 1503 Physics (including Acoustics, Atomic Processing, Informational Sciences, Information Technology, Management Information Systems) 1901 Biological

  17. DOEs Effort to Reduce Truck Aerodynamic Drag through Joint...

    Energy Savers [EERE]

    3 DOE Hydrogen and Fuel Cells Program and Vehicle Technologies Program Annual Merit Review and Peer Evaluation Meeting vss006salari2013o.pdf More Documents & Publications...

  18. Active Aerodynamic Blade Control Design for Load Alleviation on Large Wind Turbines for Increased Energy Capture

    Broader source: All U.S. Department of Energy (DOE) Office Webpages (Extended Search)

    AFDC Printable Version Share this resource Send a link to EERE: Alternative Fuels Data Center Home Page to someone by E-mail Share EERE: Alternative Fuels Data Center Home Page on Facebook Tweet about EERE: Alternative Fuels Data Center Home Page on Twitter Bookmark EERE: Alternative Fuels Data Center Homesum_a_epg0_fpd_mmcf_m.xls" ,"Available from WebQuantity ofkandz-cm11 OutreachProductswsicloudwsicloudden DocumentationAccommodationsRegister / Vol. 72, No. 39 1S1!4T op Document:

  19. Comments on: Aerodynamic Wind-Turbine Blade Design for the National Rotor

    Broader source: All U.S. Department of Energy (DOE) Office Webpages (Extended Search)

    AFDC Printable Version Share this resource Send a link to EERE: Alternative Fuels Data Center Home Page to someone by E-mail Share EERE: Alternative Fuels Data Center Home Page on Facebook Tweet about EERE: Alternative Fuels Data Center Home Page on Twitter Bookmark EERE: Alternative Fuels Data Center Homesum_a_epg0_fpd_mmcf_m.xls" ,"Available from WebQuantity ofkandz-cm11 OutreachProductswsicloudwsiclouddenDVA N C E D BGene NetworkNuclearDNP

  20. DOE's effort to reduce truck aerodynamic drag through joint experiments and

    Office of Scientific and Technical Information (OSTI)

    AFDC Printable Version Share this resource Send a link to EERE: Alternative Fuels Data Center Home Page to someone by E-mail Share EERE: Alternative Fuels Data Center Home Page on Facebook Tweet about EERE: Alternative Fuels Data Center Home Page on Twitter Bookmark EERE: Alternative Fuels Data Center Homesum_a_epg0_fpd_mmcf_m.xls" ,"Available from WebQuantity of NaturalDukeWakefieldSulfate Reducing BacteriaConnect Collidertransfer (Journal Article) |Programs ofReportcomputations.

  1. Aerodynamic drag reduction apparatus for gap-divided bluff bodies such as

    Office of Scientific and Technical Information (OSTI)

    AFDC Printable Version Share this resource Send a link to EERE: Alternative Fuels Data Center Home Page to someone by E-mail Share EERE: Alternative Fuels Data Center Home Page on Facebook Tweet about EERE: Alternative Fuels Data Center Home Page on Twitter Bookmark EERE: Alternative Fuels Data Center Homesum_a_epg0_fpd_mmcf_m.xls" ,"Available from WebQuantity of NaturalDukeWakefield MunicipalTechnicalInformation4563Abuse Tolerance(Conference)Geothermal

  2. Aerodynamic drag reduction apparatus for gap-divided bluff bodies such as

    Office of Scientific and Technical Information (OSTI)

    AFDC Printable Version Share this resource Send a link to EERE: Alternative Fuels Data Center Home Page to someone by E-mail Share EERE: Alternative Fuels Data Center Home Page on Facebook Tweet about EERE: Alternative Fuels Data Center Home Page on Twitter Bookmark EERE: Alternative Fuels Data Center Homesum_a_epg0_fpd_mmcf_m.xls" ,"Available from WebQuantity of NaturalDukeWakefield MunicipalTechnicalInformation4563Abuse Tolerance(Conference)Geothermaltractor-trailers (Patent) |

  3. DOEs Effort to Improve Heavy Vehicle Fuel Efficiency through Improved Aerodynamics

    Office of Energy Efficiency and Renewable Energy (EERE) Indexed Site

    AFDC Printable Version Share this resource Send a link to EERE: Alternative Fuels Data Center Home Page to someone by E-mail Share EERE: Alternative Fuels Data Center Home Page on Facebook Tweet about EERE: Alternative Fuels Data Center Home Page on Twitter Bookmark EERE: Alternative Fuels Data Center Home Page on Google Bookmark EERE: Alternative Fuels Data Center Home Page on Delicious Rank EERE:FinancingPetroleum Based| Department8, 20153 METHODSDOE/LaborSeptember 6,53197 This work was

  4. DOEs Effort to Reduce Truck Aerodynamic Drag through Joint Experiments

    Office of Energy Efficiency and Renewable Energy (EERE) Indexed Site

    AFDC Printable Version Share this resource Send a link to EERE: Alternative Fuels Data Center Home Page to someone by E-mail Share EERE: Alternative Fuels Data Center Home Page on Facebook Tweet about EERE: Alternative Fuels Data Center Home Page on Twitter Bookmark EERE: Alternative Fuels Data Center Home Page on Google Bookmark EERE: Alternative Fuels Data Center Home Page on Delicious Rank EERE:FinancingPetroleum Based| Department8, 20153 METHODSDOE/LaborSeptember 6,53197 This work wasand

  5. DOEs Effort to Reduce Truck Aerodynamic Drag through Joint Experiments

    Office of Energy Efficiency and Renewable Energy (EERE) Indexed Site

    AFDC Printable Version Share this resource Send a link to EERE: Alternative Fuels Data Center Home Page to someone by E-mail Share EERE: Alternative Fuels Data Center Home Page on Facebook Tweet about EERE: Alternative Fuels Data Center Home Page on Twitter Bookmark EERE: Alternative Fuels Data Center Home Page on Google Bookmark EERE: Alternative Fuels Data Center Home Page on Delicious Rank EERE:FinancingPetroleum Based| Department8, 20153 METHODSDOE/LaborSeptember 6,53197 This work wasandand

  6. DOEs Effort to Reduce Truck Aerodynamic Drag through Joint Experiments

    Office of Energy Efficiency and Renewable Energy (EERE) Indexed Site

    AFDC Printable Version Share this resource Send a link to EERE: Alternative Fuels Data Center Home Page to someone by E-mail Share EERE: Alternative Fuels Data Center Home Page on Facebook Tweet about EERE: Alternative Fuels Data Center Home Page on Twitter Bookmark EERE: Alternative Fuels Data Center Home Page on Google Bookmark EERE: Alternative Fuels Data Center Home Page on Delicious Rank EERE:FinancingPetroleum Based| Department8, 20153 METHODSDOE/LaborSeptember 6,53197 This work

  7. DOEs Effort to Reduce Truck Aerodynamic Drag through Joint Experiments

    Office of Energy Efficiency and Renewable Energy (EERE) Indexed Site

    AFDC Printable Version Share this resource Send a link to EERE: Alternative Fuels Data Center Home Page to someone by E-mail Share EERE: Alternative Fuels Data Center Home Page on Facebook Tweet about EERE: Alternative Fuels Data Center Home Page on Twitter Bookmark EERE: Alternative Fuels Data Center Home Page on Google Bookmark EERE: Alternative Fuels Data Center Home Page on Delicious Rank EERE:FinancingPetroleum Based| Department8, 20153 METHODSDOE/LaborSeptember 6,53197 This workand

  8. DOEs Effort to Reduce Truck Aerodynamic Drag through Joint Experiments

    Office of Energy Efficiency and Renewable Energy (EERE) Indexed Site

    AFDC Printable Version Share this resource Send a link to EERE: Alternative Fuels Data Center Home Page to someone by E-mail Share EERE: Alternative Fuels Data Center Home Page on Facebook Tweet about EERE: Alternative Fuels Data Center Home Page on Twitter Bookmark EERE: Alternative Fuels Data Center Home Page on Google Bookmark EERE: Alternative Fuels Data Center Home Page on Delicious Rank EERE:FinancingPetroleum Based| Department8, 20153 METHODSDOE/LaborSeptember 6,53197 This workandand

  9. Impact of Higher Fidelity Models on Active Aerodynamic Load Control For Fatigue Damage Reduction

    Broader source: All U.S. Department of Energy (DOE) Office Webpages (Extended Search)

    AFDC Printable Version Share this resource Send a link to EERE: Alternative Fuels Data Center Home Page to someone by E-mail Share EERE: Alternative Fuels Data Center Home Page on Facebook Tweet about EERE: Alternative Fuels Data Center Home Page on Twitter Bookmark EERE: Alternative Fuels Data Center Homesum_a_epg0_fpd_mmcf_m.xls" ,"Available from WebQuantityBonneville Power Administration would likeUniverseIMPACT EVALUATION PLAN FOR THE SITE- SPECIFIC SAVINGS PORTFOLIOImpact

  10. Sandia Energy - Aerodynamic Wind-Turbine Blade Design for the National

    Broader source: All U.S. Department of Energy (DOE) Office Webpages (Extended Search)

    AFDC Printable Version Share this resource Send a link to EERE: Alternative Fuels Data Center Home Page to someone by E-mail Share EERE: Alternative Fuels Data Center Home Page on Facebook Tweet about EERE: Alternative Fuels Data Center Home Page on Twitter Bookmark EERE: Alternative Fuels Data Center Homesum_a_epg0_fpd_mmcf_m.xls" ,"Available from WebQuantity ofkandz-cm11 Outreach Home RoomPreservation of Fe(II) byMultidayAlumni >Scientific andInstituteAdvancedAdvanced

  11. The effect of sintering and CMAS on the stability of plasma-sprayed zirconia thermal barrier coatings

    E-Print Network [OSTI]

    Shinozaki, Maya

    2013-07-09

    . The vapour evaporates according to a cosn characteristic in all areas of the chamber. The vapour of the coating material condenses onto a (preheated) substrate surface, forming a coating. If an oxide is being deposited, a controlled amount of oxygen may... . This has obvious aerodynamic advantages and eliminates the need for final polishing stages. In addition, the EB-PVD process deposits with minimal closure of cooling holes (0.25 0.5 mm diameter) in aerofoils and therefore requires less subsequent...

  12. Fluid--Structure Interaction : : Physiologic Simulation of Pulsatile Ventricular Assist Devices using Isogeometric Analysis

    E-Print Network [OSTI]

    Long, Christopher Curtis

    2013-01-01

    simulation of wind turbine aerodynamics: Validation studyand Y. Bazilevs. Wind turbine aerodynamics using ALEVMS:routinely used for wind turbine aerodynamics [21, 76, 78

  13. TRIGEMINAL UPTAKE AND CLEARANCE OF INHALED MANGANESECHLORIDE IN RATS AND MICE

    SciTech Connect (OSTI)

    Lewis, J; Bench, G; Myers, O; Tinner, B; Staines, W; Barr, E; Divine, K K; Barrington, W; Karlsson, J

    2003-12-09

    Inhaled manganese (Mn) can enter the olfactory bulbs via the olfactory epithelium, and can then be further transported trans-synaptically to deeper brain structures. In addition to olfactory neurons, the nasal cavity is innervated by the maxillary division of the trigeminal nerve that projects to the spinal trigeminal nucleus. Direct uptake and transport of inhaled metal particles in the trigeminal system has not been investigated previously. We studied the uptake, deposition, and clearance of soluble Mn in the trigeminal system following nose-only inhalation of environmentally relevant concentrations. Rats and mice were exposed for 10 days (6 hours/day, 5 days/week) to air or MnCl2 aerosols containing 2.3 {+-} 1.3mg Mn/m{sup 3} with mass median aerodynamic diameter (MMAD) of 3.1 {+-} 1.4 {micro}m for rats and 2.0 {+-} 0.09 mg Mn/m{sup 3} MnCl{sup 2} with MMAD of 1.98 {+-} 0.12 {micro}m for mice. Mn concentrations in the trigeminal ganglia and spinal trigeminal nucleus were measured 2 hours (0 day), 7, 14, or 30 days post-exposure using Proton Induced X-ray Emission (PIXE). Manganese-exposed rats and mice showed statistically elevated levels of Mn in trigeminal ganglia 0, 7 and 14 days after the 10 day exposure period when compared to control animals. The Mn concentration gradually decreased over time with a clearance rate (t{sub 1/2}) of 7-8 days. Rats and mice were similar in both average accumulated Mn levels in trigeminal ganglia and in rates of clearance. We also found a small but significant elevation of Mn in the spinal trigeminal nucleus of mice 7 days post-exposure and in rats 0 and 7 days post-exposure. Our data demonstrate that the trigeminal nerve can serve as a pathway for entry of inhaled Mn to the brain in rodents following nose-only exposure and raise the question of whether entry of toxicants via this pathway may contribute to development of neurodegenerative diseases.

  14. SIZE DISTRIBUTION AND RATE OF PRODUCTION OF AIRBORNE PARTICULATE MATTER GENERATED DURING METAL CUTTING

    SciTech Connect (OSTI)

    M.A. Ebadian, Ph.D.; S.K. Dua, Ph.D., C.H.P.; Hillol Guha, Ph.D.

    2001-01-01

    During deactivation and decommissioning activities, thermal cutting tools, such as plasma torch, laser, and gasoline torch, are used to cut metals. These activities generate fumes, smoke and particulates. These airborne species of matter, called aerosols, may be inhaled if suitable respiratory protection is not used. Inhalation of the airborne metallic aerosols has been reported to cause ill health effects, such as acute respiratory syndrome and chromosome damage in lymphocytes. In the nuclear industry, metals may be contaminated with radioactive materials. Cutting these metals, as in size reduction of gloveboxes and tanks, produces high concentrations of airborne transuranic particles. Particles of the respirable size range (size < 10 {micro}m) deposit in various compartments of the respiratory tract, the fraction and the site in the respiratory tract depending on the size of the particles. The dose delivered to the respiratory tract depends on the size distribution of the airborne particulates (aerosols) and their concentration and radioactivity/toxicity. The concentration of airborne particulate matter in an environment is dependent upon the rate of their production and the ventilation rate. Thus, measuring aerosol size distribution and generation rate is important for (1) the assessment of inhalation exposures of workers, (2) the selection of respiratory protection equipment, and (3) the design of appropriate filtration systems. Size distribution of the aerosols generated during cutting of different metals by plasma torch was measured. Cutting rates of different metals, rate of generation of respirable mass, as well as the fraction of the released kerf that become respirable were determined. This report presents results of these studies. Measurements of the particles generated during cutting of metal plates with a plasma arc torch revealed the presence of particles with mass median aerodynamic diameters of particles close to 0.2 {micro}m, arising from condensation of vaporized material and subsequent rapid formation of aggregates. Particles of larger size, resulting from ejection of melted material or fragments from the cutting zone, were also observed. This study presents data regarding the metal cutting rate, particle size distribution, and their generation rate, while using different cutting tools and metals. The study shows that respirable particles constitute only a small fraction of the released kerf.

  15. The design of a reduced diameter Pebble Bed Modular Reactor for reactor pressure vessel transport by railcar

    E-Print Network [OSTI]

    Everson, Matthew S

    2009-01-01

    Many desirable locations for Pebble Bed Modular Reactors are currently out of consideration as construction sites for current designs due to limitations on the mode of transportation for large RPVs. In particular, the ...

  16. Optical micrograph of a Bragg grating photodeposited in the cladding of a 180 m diameter optical fiber

    E-Print Network [OSTI]

    Wolberg, George

    fiber Grating: 5-6 m lines, 8 m spaces Inserts and removes light from fiber core d variable porosity and truck trailers or retrofitted into existing units, these sensors offer rapid, noninvasive analytical on the subject of optical biopsy. Optical biopsy involves the use of light and photonic technology to diagnose

  17. The effects of plate thickness and perforation diameter on the supporting vapor velocity for a perforated plate fractionating column

    E-Print Network [OSTI]

    Cottle, John Ernest

    1948-01-01

    &opere poser t-t vari, bio "ransformr. i oo t'. t t!ie ! o-t oii-'? it to ! h liquiu could bo adeustod. "'nis rran, cmont per&aitted t. '. o, . inc. &&ance of t. '. e li&;uid temp rature t iCG P plus or minus 0, 1 P. all liquid aial air temperatures of tlic... without bio"!in, the liquid out of the ma&master and the connections available leaked. Since the plate pressure drop was unimportant ~?ay~, tne manometer was ab ndoned after the first fow r&&ns were mode. In a commercial oolumn r&here liquid...

  18. Thermo-Physical Modeling of W.I.S.E. Observed Asteroids; Determining the Diameter and Investigating the Yarkovsky Effect

    E-Print Network [OSTI]

    California at Los Angles, University of

    depleted through collisions and by ejection into the inner solar system while simultaneously being determined. 1 Introduction The largest population of Asteroid's in the inner solar system is the main belt population of solar sys- tem bodies known as near-Earth objects (NEOs), which are asteroids and comets

  19. The effects of two different environments upon the density, diameter, and length of the hair of Brahman cattle

    E-Print Network [OSTI]

    De Armas, Hector

    1952-01-01

    twofold effect upon the efficiency' of bovine productiont the stimulation of metabolism and tissues ands to some extent, , a sterilising influence (Bonsma, 19/8) Therefore, animal husbandry research workers had to determine which genetic...

  20. Nucleation of single GaN nanorods with diameters smaller than 35 nm by molecular beam epitaxy

    SciTech Connect (OSTI)

    Chen, Yen-Ting [Institute of Atomic and Molecular Sciences, Academia Sinica, 10617 Taipei, Taiwan (China) [Institute of Atomic and Molecular Sciences, Academia Sinica, 10617 Taipei, Taiwan (China); Department of Physics, Chemistry and Biology (IFM), Linkping University, S-58183 Linkping (Sweden); Araki, Tsutomu [Department of Electrical and Electronic Engineering, Ritsumeikan University, 525-8577 Shiga (Japan)] [Department of Electrical and Electronic Engineering, Ritsumeikan University, 525-8577 Shiga (Japan); Palisaitis, Justinas; Persson, Per O. .; Olof Holtz, Per; Birch, Jens [Department of Physics, Chemistry and Biology (IFM), Linkping University, S-58183 Linkping (Sweden)] [Department of Physics, Chemistry and Biology (IFM), Linkping University, S-58183 Linkping (Sweden); Chen, Li-Chyong [Center for Condensed Matter Sciences, National Taiwan University, 10617 Taipei, Taiwan (China)] [Center for Condensed Matter Sciences, National Taiwan University, 10617 Taipei, Taiwan (China); Chen, Kuei-Hsien [Institute of Atomic and Molecular Sciences, Academia Sinica, 10617 Taipei, Taiwan (China) [Institute of Atomic and Molecular Sciences, Academia Sinica, 10617 Taipei, Taiwan (China); Center for Condensed Matter Sciences, National Taiwan University, 10617 Taipei, Taiwan (China); Nanishi, Yasushi [Global Innovation Research Organization, Ritsumeikan University, 525-8577 Shiga (Japan)] [Global Innovation Research Organization, Ritsumeikan University, 525-8577 Shiga (Japan)

    2013-11-11

    Nucleation mechanism of catalyst-free GaN nanorod grown on Si(111) is investigated by the fabrication of uniform and narrow (<35 nm) nanorods without a pre-defined mask by molecular beam epitaxy. Direct evidences show that the nucleation of GaN nanorods stems from the sidewall of the underlying islands down to the Si(111) substrate, different from commonly reported ones on top of the island directly. Accordingly, the growth and density control of the nanorods is exploited by a narrow-pass approach that only narrow nanorod can be grown. The optimal size of surrounding non-nucleation area around single nanorod is estimated as 88 nm.

  1. Measurements versus Predictions for a Hybrid (Hydrostatic plus Hydrodynamic Thrust Bearing for a Range of Orifice Diameters

    E-Print Network [OSTI]

    Esser, Paul R.

    2011-08-08

    the static axial load, which is reacted by a second thrust bearing. The rotor is supported radially by two water-lubricated fluid film journal bearings and is attached to a 30,600 rpm motor via a high speed coupling with very low axial stiffness. Thrust...

  2. Theoretical and empirical study of single-substance, upward two-phase flow in a constant-diameter adiabatic pipe

    SciTech Connect (OSTI)

    Laoulache, R.N.; Maeder, P.F.; DiPippo, R.

    1987-05-01

    A Scheme is developed to describe the upward flow of a two-phase mixture of a single substance in a vertical adiabatic constant area pipe. The scheme is based on dividing the mixture into a homogeneous core surrounded by a liquid film. This core may be a mixture of bubbles in a contiguous liquid phase, or a mixture of droplets in a contiguous vapor phase. Emphasis is placed upon the latter case since the range of experimental measurements of pressure, temperature, and void fraction collected in this study fall in the slug-churn''- annular'' flow regimes. The core is turbulent, whereas the liquid film may be laminar or turbulent. Turbulent stresses are modeled by using Prandtl's mixing-length theory. The working fluid is Dichlorotetrafluoroethane CCIF{sub 2}-CCIF{sub 2} known as refrigerant 114 (R-114); the two-phase mixture is generated from the single phase substance by the process of flashing. In this study, the effect of the Froude and Reynolds numbers on the liquid film characteristics is examined. The compressibility is accounted for through the acceleration pressure gradient of the core and not directly through the Mach number. An expression for an interfacial friction coefficient between the turbulent core and the liquid film is developed; it is similar to Darcy's friction coefficient for a single phase flow in a rough pipe. Finally, an actual steam-water geothermal well is simulated; it is based on actual field data from New Zealand. A similarity theory is used to predict the steam-water mixture pressure and temperature starting with laboratory measurements on the flow of R-114.

  3. Development of Larger Diameter High Pressure CNG Cylinder Manufactured by Piercing and Drawing for Natural Gas Vehicle

    Office of Energy Efficiency and Renewable Energy (EERE)

    These slides were presented at the International Hydrogen Fuel and Pressure Vessel Forum on September 27 29, 2010, in Beijing, China.

  4. Status report. Characterization of Weld Residual Stresses on a Full-Diameter SNF Interim Storage Canister Mockup.

    SciTech Connect (OSTI)

    Enos, David; Bryan, Charles R.

    2015-08-01

    This report documents the mockup specifications and manufacturing processes; the initial cutting of the mockup into three cylindrical pieces for testing and the measured strain changes that occurred during the cutting process; and the planned weld residual stress characterization activities and the status of those activities.

  5. Heavy duty insulator assemblies for 500-kV bulk power transmission line with large diameter octagonalbundled conductor

    SciTech Connect (OSTI)

    Tsujimoto, K.; Hayase, I.; Hirai, J.; Inove, M.; Naito, K.; Yukino, T.

    1982-11-01

    This paper describes the design procedure and the results of field tests on mechanical performances of insulator assemblies newly developed to support octagonal-bundled conductors for 500-kV bulk power transmission. Taking account of conductor-motion-induced peak tensile load, fatigue, torsional torque and others, a successful design has been achieved in two prototype assemblies for such heavy mechanical duties as encountered during conductor galloping or swing. This has been proved throughout three years of the field tests.

  6. Nearly Exclusive Growth of Small Diameter Semiconducting Single-Wall Carbon Nanotubes from Organic Chemistry Synthetic End-Cap

    E-Print Network [OSTI]

    Zhou, Chongwu

    spectroscopic characterization, electrical transport measurements, and density functional theory calculations for Energy and Resources, The University of Newcastle, Callaghan 2308, Australia WPI to achieve high-efficiency metal-free growth of nearly pure SWCNT semiconductors, as supported by extensive

  7. ORIGINAL PAPER Sustainability metrics for eco-technologies assessment, Part II.

    E-Print Network [OSTI]

    Grossmann, Ignacio E.

    . Additional sustainability indexes are evaluated: material index, energy index, and ecoefficiency. The results in route i (kg) C Equipment cost (US$) Fc Correction factor H Equipment height (ft) D Equipment diameter (ft) M&S Marshall and Swift index A Heat transfer area (ft2 ) LD50 Median lethal dose M Material index

  8. ECOHYDROLOGY Ecohydrol. 3, 497508 (2010)

    E-Print Network [OSTI]

    Lehmann, Johannes

    2010-01-01

    transport in soil greatly influences its stability, the dynamics of soil microbial communities and organic. The particles larger than 54% of median grain diameter were filtered out of suspension during passage through to other types of colloids, this study highlights the importance of pH, IS, particle size, and soil water

  9. Bed-Material Load Computations for Nonuniform Sediments Baosheng Wu, M.ASCE1

    E-Print Network [OSTI]

    Julien, Pierre Y.

    Bed-Material Load Computations for Nonuniform Sediments Baosheng Wu, M.ASCE1 ; Albert Molinas, M developed for single particle sizes improves the accuracy of transport calculations for sediment mixtures.5. Sediment in transport also follows a lognormal distribution with a median diameter d50t generally finer

  10. CLOUD MICROPHYSICAL PROPERTIES, PROCESSES, AND RAINFALL ESTIMATION OPPORTUNITIES

    E-Print Network [OSTI]

    Daniel, Rosenfeld

    , and a formulation of the RDSD into the simplest free parameters of the rain intensity R, rain water content W intensity R, rain water content W and median volume drop diameter D0. This is accomplished through-R relationships is explored from the combined approach of rain-forming physical processes that shape the RDSD

  11. Extending the Capabilities of Single Particle Mass Spectrometry: II. Measurements of Aerosol Particle Density without DMA

    SciTech Connect (OSTI)

    Vaden, Timothy D.; Imre, D.; Beranek, Josef; Zelenyuk, Alla

    2011-01-04

    Particle density is an important and useful property that is difficult to measure because it usually 5 requires separate instruments to measure two particle attributes. As density measurements are 6 often performed on size-classified particles, they are hampered by low particle numbers, and 7 hence poor temporal resolution. We present here a new method for measuring particle densities 8 using our single particle mass spectrometer, SPLAT. This method takes advantage of the fact 9 that the detection efficiency in our single particle mass spectrometer drops off very rapidly as the 10 particle size decreases below ~125 nm creating a distinct sharp feature on the small particle side 11 of the vacuum aerodynamic size distribution. Thus, the two quantities needed to determine 12 particle density, the particle diameter and vacuum aerodynamic diameter, are known. We first 13 test this method on particles of known composition and find that the densities it yields are 14 sufficiently accurate. We then apply the method to obtain the densities of particles that were 15 characterized during an airborne field campaign. In addition, we show that the distinctive 16 features of the vacuum aerodynamic size distribution can be used to characterize the instrument 17 detection efficiency as a function of particle size. In general, the method presented here reduces 18 complexity and yields information with high temporal resolution while the instrument is 19 collecting routine data on particle size and composition.

  12. nATuRE CommunICATIons | 3:615 | DoI: 10.1038/ncomms1630 | www.nature.com/naturecommunications 2012 Macmillan Publishers Limited. All rights reserved.

    E-Print Network [OSTI]

    Daraio, Chiara

    and aerodynamic surfaces from aviation to wind turbine industries4,5. Ice accumulation on aerodynamic wing

  13. Low-Maintenance Wind Power System

    E-Print Network [OSTI]

    Rasson, Joseph E

    2010-01-01

    Improved Vertical Axis Wind Turbine and Aerodynamic ControlDarrieus Vertical Axis Wind Turbines and Aerodynamic Control

  14. unsteady aerodynamic and hydrodynamic forces and structural dynamics such as power take-off and control system responses.

    E-Print Network [OSTI]

    -fidelity large-eddy simulation model that simulates wind and water inflows that occur in offshore wind farms-off and control system responses. Offshore Wind Modeling Researchers at NREL have developed a new complex modeling and analysis tool capable of analyzing floating platform concepts for offshore wind turbines. The new modeling

  15. Investigation of Dynamic Aerodynamics and Control of Wind Turbine Sections Under Relevant Inflow/Blade Attitude Conditions

    SciTech Connect (OSTI)

    Naughton, Jonathan W.

    2014-08-05

    The growth of wind turbines has led to highly variable loading on the blades. Coupled with the relative reduced stiffness of longer blades, the need to control loading on the blades has become important. One method of controlling loads and maximizing energy extraction is local control of the flow on the wind turbine blades. The goal of the present work was to better understand the sources of the unsteady loading and then to control them. This is accomplished through an experimental effort to characterize the unsteadiness and the effect of a Gurney flap on the flow, as well as an analytical effort to develop control approaches. It was planned to combine these two efforts to demonstrate control of a wind tunnel test model, but that final piece still remains to be accomplished.

  16. Aerodynamic characteristics of a feathered dinosaur measured using physical models. Effects of form on static stability and control effectiveness

    E-Print Network [OSTI]

    Evangelista, Dennis

    2013-01-01

    models constructed from styrofoam gliders, to test thebetween lead and styrofoam. Our predicted equilibrium glide

  17. A robust simplex cut-cell method for adaptive high-order discretizations of aerodynamics and multi-physics problems

    E-Print Network [OSTI]

    Sun, Huafei

    2013-01-01

    Despite the wide use of partial differential equation (PDE) solvers, lack of automation still hinders realizing their full potential in assisting engineering analysis and design. In particular, the process of establishing ...

  18. 44rd Aerospace Sciences Meeting, January 9-12,2006, Reno,NV Aerodynamic Simulation and Shape Optimization for

    E-Print Network [OSTI]

    Jameson, Antony

    algorithms for unstructured meshes, represented by the Airplane Code, and on adjoint based optimization techniques. It seems a particularly opportune moment to review the Airplane Code, because we originally at this Symposium. While much of Boggy's research was focused on experimental studies of supersonic shock wave

  19. Aerodynamics (4 units) Class/Laboratory Schedule: four lecture hours per week, three lab, and five hours outside

    E-Print Network [OSTI]

    Fainman, Yeshaiahu

    and bodies at subsonic and supersonic speeds. Thin-wing theory. Slender-body theory. Formulation of theories for the evaluation of forces and moments on airplane geometries. Application to the design of high-speed airplanes principles of the design of airplane components 4.2 Students will demonstrate the ability to apply principles

  20. A Computational Method for Determining Distributed Aerodynamic Loads on Planforms of Arbitrary Shape in Compressible Subsonic Flow

    E-Print Network [OSTI]

    Brown, Matthew Alan

    2013-12-31

    of the cranked wing approach, most planforms can be modeled including nearly all practical lifting surfaces with some notable exceptions. The methods are extremely accurate for elliptic wings and rectangular wings with some notable difficulty attributed to swept...