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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)

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 ...

Williams, L. R.

2

AEROSPACE SCIENCES Applied aerodynamics  

E-Print Network (OSTI)

AEROSPACE SCIENCES Applied aerodynamics This year saw significant progress in industry, research labs, and academia in the development of flow-control concepts, novel configuration aerodynamic concepts, and aerodynamic im- provement technologies for enhancing the fuel efficiency and performance

Xu, Kun

3

Neo Aerodynamic | Open Energy Information  

Open Energy Info (EERE)

Neo Aerodynamic Jump to: navigation, search Name: Neo Aerodynamic Region: United States Sector: Marine and Hydrokinetic Website: http:www.neo-aerodynamic.com This company is...

4

Aerodynamics Antony Jameson  

E-Print Network (OSTI)

Chapter 11 Aerodynamics Antony Jameson Stanford University, Stanford, CA, USA 1 Focus Multidimensional Domains 359 6 Time-stepping Schemes 365 7 Aerodynamic Shape Optimization 379 8 Related Chapters 400 Acknowledgment 400 References 400 1 FOCUS AND HISTORICAL BACKGROUND 1.1 Classical aerodynamics

Jameson, Antony

5

The Aerodynamic Forces On Misaligned Platoons  

E-Print Network (OSTI)

M. , Tokumaru, P. , 1997, “Aerodynamic benefits from close-Mason, W.T. , (Ed. ): Aerodynamic Drag Mechanisms of BluffBrowand, F. , 1995, The aerodynamic performance of platoons;

Marcu, Bogdan; Browand, Fred

1998-01-01T23:59:59.000Z

6

Aerodynamic interference between two Darrieus wind turbines  

SciTech Connect

The effect of aerodynamic interference on the performance of two curved bladed Darrieus-type vertical axis wind turbines has been calculated using a vortex/lifting line aerodynamic model. The turbines have a tower-to-tower separation distance of 1.5 turbine diameters, with the line of turbine centers varying with respect to the ambient wind direction. The effects of freestream turbulence were neglected. For the cases examined, the calculations showed that the downwind turbine power decrement (1) was significant only when the line of turbine centers was coincident with the ambient wind direction, (2) increased with increasing tipspeed ratio, and (3) is due more to induced flow angularities downstream than to speed deficits near the downstream turbine.

Schatzle, P.R.; Klimas, P.C.; Spahr, H.R.

1981-04-01T23:59:59.000Z

7

AIAA 20033498 Viscous Aerodynamic Shape  

E-Print Network (OSTI)

AIAA 2003­3498 Viscous Aerodynamic Shape Optimization of Wings including Planform Variables Kasidit Aerodynamics Conference Orlando, Florida/June 23­26, 2003 For permission to copy or republish, contact­4344 #12;VISCOUS AERODYNAMIC SHAPE OPTIMIZATION OF WINGS INCLUDING PLANFORM VARIABLES Kasidit Leoviriyakit

Jameson, Antony

8

Field Study on PM1 Air Pollution in a Residential Underground Parking Lot  

Science Journals Connector (OSTI)

PM1 (fine particles with a diameter smaller than 1 ?m) number concentrations are more straightforward compared with particle mass concentrations for air quality assessment in underground parking lots. PM1 ... PM1...

Yu Zhao; Jianing Zhao

2014-01-01T23:59:59.000Z

9

Aerodynamic Analysis of wind turbine.  

E-Print Network (OSTI)

??The thesis investigates the application of vortex theory for analyzing the aerodynamic loads on wind turbine blades. Based on this method, a graphical user friendly… (more)

Zarmehri, Ayyoob

2012-01-01T23:59:59.000Z

10

Low Speed Unsteady Aerodynamics Soumitra Banerjee*  

E-Print Network (OSTI)

Low Speed Unsteady Aerodynamics Soumitra Banerjee* Virginia Polytechnic Institute and State University, Blacksburg, Virginia, 24061 Unsteady aerodynamics is the study of fluid flow, where the flow field changes with time. The unsteadiness is significant in many aerodynamic applications; few examples

Patil, Mayuresh

11

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

12

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...

13

Modelling and Simulation in Aerodynamic Design  

E-Print Network (OSTI)

Modelling and Simulation in Aerodynamic Design In different kinds of aerodynamic design elements is too complex. Aerodynamic properties of different airfoils are found from either numerical turbine blade, two design features are important. The aerodynamic design attempts to optimize the blade

Mosegaard, Klaus

14

Aerodynamics at the Particle Level  

E-Print Network (OSTI)

This paper is intended to clarify some of the rather well-known aerodynamic phenomena. It is also intended to pique the interest of the layman as well as the professional. All aerodynamic forces on a surface are caused by collisions of fluid particles with the surface. While the standard approach to fluid dynamics, which is founded on the fluid approximation, is effective in providing a means of calculating various behavior and properties, it begs the question of causality. The determination of the causes of many of the most important aerodynamic effects requires a microscopic examination of the fluid and of the surface with which it interacts. The Kutta-Joukowski theorem is investigated from first physical principles. It is noted that the circulation does not arise as a physical phenomenon. Various aerodynamic devices are discussed, e.g. rocket engine exhaust diffuser and the perfume atomizer.

Charles A. Crummer

2012-09-23T23:59:59.000Z

15

UPWIND, Aerodynamics and aero-elasticity Rotor aerodynamics in atmospheric shear flow  

E-Print Network (OSTI)

UPWIND, Aerodynamics and aero-elasticity Rotor aerodynamics in atmospheric shear flow Niels N codes for wind turbines utilize aerodynamics based on BEM methods, see [1, 2]. For modern large scale

16

Explanation and discovery in aerodynamics  

E-Print Network (OSTI)

The purpose of this paper is to discuss and clarify the explanations commonly cited for the aerodynamic lift generated by a wing, and to then analyse, as a case study of engineering discovery, the aerodynamic revolutions which have taken place within Formula 1 in the past 40 years. The paper begins with an introduction that provides a succinct summary of the mathematics of fluid mechanics.

Gordon McCabe

2005-12-22T23:59:59.000Z

17

Transient Vehicle Aerodynamics In Four-car Platoons  

E-Print Network (OSTI)

7 Platoon Aerodynamics 7.1 Drag Coefficient . . . . . . . .0 . Savaa. Transient aerodynamics in vehicle interactions:implications in platoon aerodynamics. Master’s thesis,

Chen, A. L.; Savas, Omer; Hedrick, Karl

1997-01-01T23:59:59.000Z

18

The Aerodynamic Performance Of Platoons: A Final Report  

E-Print Network (OSTI)

OF CALIFORNIA, BERKELEY The Aerodynamic Performance of1995 ISSN 1055-1425 The Aerodynamic Performance of Platoons10 October 1995 The Aerodynamic Performance of Platoons A

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

1995-01-01T23:59:59.000Z

19

The Aerodynamics of Deforming Wings at Low Reynolds Number  

E-Print Network (OSTI)

and Karl G. Gotz. Unsteady aerodynamic performance of model26] G. Du and M. Sun. Aerodynamic effects of corrugation andof flexibility on the aerodynamic performance of a hovering

Medina, Albert

2013-01-01T23:59:59.000Z

20

LL Pm  

Office of Legacy Management (LM)

LL LL Pm ' F II c iJr Fa, i n m n ys m * t F t F c* F F -- ORAU 89/G-77 IL. 17- Prepared by Oak Ridge Associated Universities Prepared for Division of Facility and Site Decommissioning U.S. Department of Energy RADIOLOGICAL SURVEY AT 18 HENDERSON STREET JOLIET, ILLINOIS M. R. LANDIS Environmental Survey and Site Assessment Program Energy/Environment Systems Division FINAL REPORT OCTOBER 1989 . rlly mfhct Ez of the 8pmnmtng Institutiona of Oak Ridga Asaodatd ThsoplnlonBoxpmnsdhDrDlndonotnnasn IJnm T~~m~rdnM~ofvrorks~byt~Unk~S~~ Gowmmat. N&her tha Unltd States Govsmmmrtl nor~US.~punmtatErmpy,nor8nyof~r~plqow.nw)cn~w~,orpm~orknplkd,oruruma~y~8Ii~bUby or msponslbUlty lor tlu sccumcy. complot~nass. or udutfan of my InformWon, l pparatu% product, or procow

Note: This page contains sample records for the topic "aerodynamic diameter pm" from the National Library of EnergyBeta (NLEBeta).
While these samples are representative of the content of NLEBeta,
they are not comprehensive nor are they the most current set.
We encourage you to perform a real-time search of NLEBeta
to obtain the most current and comprehensive results.


21

Spring 2011 ME706 Acoustics and Aerodynamic Sound ME706 Acoustics and Aerodynamic Sound  

E-Print Network (OSTI)

Spring 2011 ME706 Acoustics and Aerodynamic Sound ME706 Acoustics and Aerodynamic Sound Instructor-surface interaction. Spring 2011 1 ME706 Acoustics and Aerodynamic Sound #12;Spring 2011 ME706 Acoustics and Aerodynamic Sound Students are expected to: · Exhibit a level of mathematical maturity roughly equivalent

22

Influence of a humidor on the aerodynamics of baseballs  

E-Print Network (OSTI)

We investigate whether storing baseballs in a controlled humidity environment significantly affects their aerodynamic properties. To do this, we measure the change in diameter and mass of baseballs as a function of relative humidity (RH) in which the balls are stored. We then model trajectories for pitched and batted baseballs to assess the difference between those stored at 30% RH versus 50% RH. The results show that a drier baseball may be expected to curve slightly more than a humidified one for a given pitch velocity. We also find that the aerodynamics alone would add ~2 feet to the distance a moister ball is hit. However, this is compensated by a ~6 foot reduction in batted distance due to the well known change in coefficient of restitution of the ball. We discuss consequences of these results for baseball played at Coors Field in Denver, where baseballs have been stored in a humidor at 50% RH since 2002.

Edmund Meyer; John Bohn

2008-02-29T23:59:59.000Z

23

ME421. Foundations of Aerodynamics. Victor Yakhot  

E-Print Network (OSTI)

ME421. Foundations of Aerodynamics. Victor Yakhot Syllabus. Spring 2014 . 1/16, 21. Fluids;Books. 1. D. Wilcox, "Basic Fluid Mechanics". 2. J. Anderson, Fundamentals of aerodynamics. 3. V.Yakhot,, ME421. Fluid Mechanics and aerodynamics. My lecture notes. 4. I. Abbott and A. Doenhoff, Theory

Lin, Xi

24

ME421. Foundations of Aerodynamics. Victor Yakhot  

E-Print Network (OSTI)

ME421. Foundations of Aerodynamics. Victor Yakhot Syllabus. Spring 2013 . 1/17, 22. Fluids Mechanics". 2. J. Anderson, Fundamentals of aerodynamics. 3. V.Yakhot,, ME421. Fluid Mechanics and aerodynamics. My lecture notes. 4. I. Abbott and A. Doenhoff, Theory of wing sections, Dover Publications, NY

25

Conformal Mapping in Wing Aerodynamics Thomas Johnson  

E-Print Network (OSTI)

Conformal Mapping in Wing Aerodynamics Thomas Johnson June 4, 2013 Contents 1 Introduction 1 2 the first complete treatment of conformal mapping in aerodynamics. Near the beginning of the twentieth and aerodynamics. The purpose of this exposition is to give the reader an elementary intro- duction to the use

Morrow, James A.

26

Challenges and Complexity of Aerodynamic Wing  

E-Print Network (OSTI)

Chapter 1 Challenges and Complexity of Aerodynamic Wing Design Kasidit Leoviriyakit and Antony@stanford.edu and jameson@baboon.stanford.edu This paper focuses on aerodynamic design methodology. It discusses challenges and complexity of aerodynamic wing design for a transonic aircraft, which arise from the complex nature of flow

Jameson, Antony

27

Airfoil Optimization Using Practical Aerodynamic Design Requirements  

E-Print Network (OSTI)

Airfoil Optimization Using Practical Aerodynamic Design Requirements Howard P. Buckley, Beckett Y., Toronto, Ontario, M3H 5T6, Canada Practical aerodynamic design problems must balance the goal the aerodynamic constraints imposed at the off-design operating conditions to be treated explicitly. Both methods

Zingg, David W.

28

Aerodynamics and Aeroelastics, WP 2 Flemming Rasmussen  

E-Print Network (OSTI)

Aerodynamics and Aeroelastics, WP 2 Flemming Rasmussen Aeroelastic Design Wind Energy Department Risø DTU #12;WP2 Aero-dynamics and Aero-elastics OBJECTIVES 1. Development of nonlinear structural dynamic models (modeling on the micromechanical scale is input from WP3). 2. Advanced aerodynamic models

29

On Aerodynamic Design Through Multipoint Numerical Optimization  

E-Print Network (OSTI)

On Aerodynamic Design Through Multipoint Numerical Optimization Howard P. Buckley, and David WT6, Canada A multipoint optimization approach is used to solve aerodynamic design problems en integral as an objective function is demonstrated to improve aerodynamic performance over a range of on

Zingg, David W.

30

CFD-based Optimization for Automotive Aerodynamics  

E-Print Network (OSTI)

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

Dumas, Laurent

31

Comparing Aerodynamic Models for Numerical Simulation of  

E-Print Network (OSTI)

Comparing Aerodynamic Models for Numerical Simulation of Dynamics and Control of Aircraft and simulation of aircraft, yet other aerodynamics models exist that can provide more accurate results for certain simulations without a large increase in computational time. In this paper, sev- eral aerodynamics

Peraire, Jaime

32

AIAA 99--1467 LOW ORDER AERODYNAMIC  

E-Print Network (OSTI)

AIAA 99--1467 LOW ORDER AERODYNAMIC MODELS FOR AEROELASTIC CONTROL OF TURBOMACHINES K.E. Willcox, J of Aeronautics and Astronautics 1801 Alexander Bell Drive, Suite 500, Reston, VA 22091 #12; LOW ORDER AERODYNAMIC order aerodynamic model is developed for aeroelastic analysis of turbomachines. The proper or­ thogonal

Peraire, Jaime

33

Toward Practical Aerodynamic Design Through Numerical Optimization  

E-Print Network (OSTI)

Toward Practical Aerodynamic Design Through Numerical Optimization David W. Zingg, and Laura6, Canada A Newton-Krylov algorithm for aerodynamic optimization is applied to the multipoint design aerodynamic design. I. Introduction Beginning with the work of Hicks et al.1 and Hicks and Henne,2 numerical

Zingg, David W.

34

Aerodynamic Lightweight Cab Structure Components | Department...  

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

and Vehicle Technologies Program Annual Merit Review and Peer Evaluation Meeting lm060smith2012o.pdf More Documents & Publications Aerodynamic Lightweight Cab Structure...

35

Rarefaction Effects in Hypersonic Aerodynamics Vladimir V. Riabov  

E-Print Network (OSTI)

Rarefaction Effects in Hypersonic Aerodynamics Vladimir V. Riabov Department of Mathematics, and others) in aerodynamics of the probes is studied. Important kinetic effects that are specific. Keywords: DSMC method, aerodynamic coefficients, hypersonic flows, similarity parameters, torus, spinning

Riabov, Vladimir V.

36

The Aerodynamics of Deforming Wings at Low Reynolds Number  

E-Print Network (OSTI)

of advance ratio on the aerodynamics of revolving wings. J.and M. H. Dickinson. The aerodynamics of hovering flight inand Industrial Aerodynamics, 96:2093–2103, 2008. [56] D. Kim

Medina, Albert

2013-01-01T23:59:59.000Z

37

THE AERODYNAMICS OF THE BRITISH LATE TRIASSIC KUEHNEOSAURIDAE  

E-Print Network (OSTI)

THE AERODYNAMICS OF THE BRITISH LATE TRIASSIC KUEHNEOSAURIDAE by KOEN STEIN* , COLIN PALMER been limited. Here, we provide a thorough aerodynamic analysis of both genera of British kuehneosaur words: Kuehneosauridae, Diapsida, Late Triassic, glid- ing, aerodynamics. The Kuehneosauridae

Benton, Michael

38

Hybrid method for aerodynamic shape optimization in automotive industry  

E-Print Network (OSTI)

Hybrid method for aerodynamic shape optimization in automotive industry Freedeerique Muyl April 2003; accepted 4 June 2003 Abstract An aerodynamic shape optimization tool for complex industrial reasons, concerns car manufacturers. Consequently, the improvement of the aerodynamics of car shapes, more

Dumas, Laurent

39

Aerodynamic Forces on Truck Models, Including Two Trucks in Tandem  

E-Print Network (OSTI)

rear-edge shaping on the aerodynamic drag of bluff vehiclesOF CALIFORNIA, BERKELEY Aerodynamic Forces on Truck Models,TRANSIT AND HIGHWAYS Aerodynamic Forces on Truck Models,

Hammache, Mustapha; Michaelian, Mark; Browand, Fred

2001-01-01T23:59:59.000Z

40

Evaporation of Water from Particles in the Aerodynamic Lens Inlet...  

NLE Websites -- All DOE Office Websites (Extended Search)

of Water from Particles in the Aerodynamic Lens Inlet: An Experimental Study. Evaporation of Water from Particles in the Aerodynamic Lens Inlet: An Experimental Study. Abstract:...

Note: This page contains sample records for the topic "aerodynamic diameter pm" from the National Library of EnergyBeta (NLEBeta).
While these samples are representative of the content of NLEBeta,
they are not comprehensive nor are they the most current set.
We encourage you to perform a real-time search of NLEBeta
to obtain the most current and comprehensive results.


41

Aerodynamic Drag and Gyroscopic Stability  

E-Print Network (OSTI)

This paper describes the effects on aerodynamic drag of rifle bullets as the gyroscopic stability is lowered from 1.3 to 1.0. It is well known that a bullet can tumble for stability less than 1.0. The Sierra Loading Manuals (4th and 5th Editions) have previously reported that ballistic coefficient decreases significantly as gyroscopic stability, Sg, is lowered below 1.3. These observations are further confirmed by the experiments reported here. Measured ballistic coefficients were compared with gyroscopic stabilities computed using the Miller Twist Rule for nearly solid metal bullets with uniform density and computed using the Courtney-Miller formula for plastic-tipped bullets. The experiments reported here also demonstrate a decrease in aerodynamic drag near Sg = 1.23 +/- 0.02. It is hypothesized that this decrease in drag over a narrow band of Sg values is due to a rapid damping of coning motions (precession and nutation). Observation of this drag decrease at a consistent value of Sg demonstrates the relati...

Courtney, Elya R

2013-01-01T23:59:59.000Z

42

The External Aerodynamics of Canine Olfaction Gary S. Settles*  

E-Print Network (OSTI)

The External Aerodynamics of Canine Olfaction Gary S. Settles* , Douglas A. Kester** , Lori J Literature on the External Aerodynamics of Olfaction B. Precedent Literature on Aerodynamic Sampling Technology III. Canine Olfaction Experiments IV. The Design of an Aerodynamic Sniffer A. Background B

Settles, Gary S.

43

Aeroelastic Analysis of Bridges: Effects of Turbulence and Aerodynamic Nonlinearities  

E-Print Network (OSTI)

Aeroelastic Analysis of Bridges: Effects of Turbulence and Aerodynamic Nonlinearities Xinzhong Chen for capturing the emerging concerns in bridge aerodynamics introduced by aerodynamic nonlinearities/or with aerodynamic characteristics sensitive to the effective angle of incidence. This paper presents a nonlinear

Kareem, Ahsan

44

MULTITARGET ERROR ESTIMATION AND ADAPTIVITY IN AERODYNAMIC FLOW SIMULATIONS  

E-Print Network (OSTI)

MULTI­TARGET ERROR ESTIMATION AND ADAPTIVITY IN AERODYNAMIC FLOW SIMULATIONS RALF HARTMANN # Abstract. Important quantities in aerodynamic flow simulations are the aerodynamic force coe subject classifications. 65N12,65N15,65N30 1. Introduction. In aerodynamic computations like compressible

Hartmann, Ralf

45

MULTITARGET ERROR ESTIMATION AND ADAPTIVITY IN AERODYNAMIC FLOW SIMULATIONS  

E-Print Network (OSTI)

MULTITARGET ERROR ESTIMATION AND ADAPTIVITY IN AERODYNAMIC FLOW SIMULATIONS RALF HARTMANN Abstract. Important quantities in aerodynamic flow simulations are the aerodynamic force coefficients including Navier-Stokes equations AMS subject classifications. 65N12,65N15,65N30 1. Introduction. In aerodynamic

Hartmann, Ralf

46

The aerodynamics of the beautiful game  

E-Print Network (OSTI)

We consider the aerodynamics of football, specifically, the interaction between a ball in flight and the ambient air. Doing so allows one to account for the characteristic range and trajectories of balls in flight, as well ...

Bush, John W. M.

2013-01-01T23:59:59.000Z

47

Anisotropic Grid Adaptation for Multiple Aerodynamic Outputs  

E-Print Network (OSTI)

Anisotropic grid–adaptive strategies are presented for viscous flow simulations in which the accurate prediction of multiple aerodynamic outputs (such as the lift, drag, and moment coefficients) is required from a single ...

Venditti, David A.

48

Transient Platoon Aerodynamics During Passing Maneuvers and In-line Oscillations  

E-Print Network (OSTI)

p CHAPTER TRANSIENT AERODYNAMICS DURING IN-LINE OSCILLATIONSA. J. , Road Vehicle Aerodynamics, Pentech Press, London,6] Hucho, W. - H . (ed. ), Aerodynamics of Road Vehicles,

Tsuei, J. L.; Savas, O.; Hedrick, J. K.

2000-01-01T23:59:59.000Z

49

Aerodynamic Drag and Gyroscopic Stability  

E-Print Network (OSTI)

This paper describes the effects on aerodynamic drag of rifle bullets as the gyroscopic stability is lowered from 1.3 to 1.0. It is well known that a bullet can tumble for stability less than 1.0. The Sierra Loading Manuals (4th and 5th Editions) have previously reported that ballistic coefficient decreases significantly as gyroscopic stability, Sg, is lowered below 1.3. These observations are further confirmed by experiments reported here. Measured ballistic coefficients were compared with gyroscopic stabilities computed using the Miller Twist Rule for nearly solid metal bullets with uniform density and computed using the Courtney-Miller formula for plastic-tipped bullets. The relationship between Sg and drag may be used to test the applicability of existing gyroscopic stability formulas for given bullet designs and to evaluate the accuracy of alternate formulas in cases where the existing stability formulas are not as accurate. The most definitive test of formulas predicting stability will always be observation of whether bullets tumble under given conditions. However, observations of drag changes provide valuable supplemental information because they suggest changes in stability as conditions change. Use of a continuous variable (drag) rather than a binary variable (tumbling) allows insight into stability over a range of conditions where the binary variable does not change.

Elya R. Courtney; Michael W. Courtney

2014-10-16T23:59:59.000Z

50

In vivo recording of aerodynamic force with an aerodynamic force platform  

E-Print Network (OSTI)

Flapping wings enable flying animals and biomimetic robots to generate elevated aerodynamic forces. Measurements that demonstrate this capability are based on tethered experiments with robots and animals, and indirect force calculations based on measured kinematics or airflow during free flight. Remarkably, there exists no method to measure these forces directly during free flight. Such in vivo recordings in freely behaving animals are essential to better understand the precise aerodynamic function of their flapping wings, in particular during the downstroke versus upstroke. Here we demonstrate a new aerodynamic force platform (AFP) for nonintrusive aerodynamic force measurement in freely flying animals and robots. The platform encloses the animal or object that generates fluid force with a physical control surface, which mechanically integrates the net aerodynamic force that is transferred to the earth. Using a straightforward analytical solution of the Navier-Stokes equation, we verified that the method is ...

Lentink, David; Ingersoll, Rivers

2014-01-01T23:59:59.000Z

51

Error estimation and adaptive mesh refinement for aerodynamic flows  

E-Print Network (OSTI)

Error estimation and adaptive mesh refinement for aerodynamic flows Ralf Hartmann1 and Paul Houston2 1 Institute of Aerodynamics and Flow Technology DLR (German Aerospace Center) Lilienthalplatz 7

Hartmann, Ralf

52

AE 400-level (choose 2): AE 410 Computational Aerodynamics  

E-Print Network (OSTI)

AE 400-level (choose 2): AE 410 Computational Aerodynamics AE 412 Viscous flow & Heat Transfer AE 416 Applied Aerodynamics AE 419 Aircraft Flight Mechanics AE 433 Aerospace Propulsion AE 434 Rocket

Gilbert, Matthew

53

Five Year Plan Update Leishman 631 Helicopter Aerodynamics I X X X X  

E-Print Network (OSTI)

2017 Rotorcraft Leishman 631 Helicopter Aerodynamics I X X X X Leishman 632 Helicopter Aerodynamics II X Aerodynamics & Propulsion Sedwick 663 Intro to Plasmas for Space Prop/Powr X X Yu 665 Advanced of Aerodynamics Jones 672 Low Reynods Number Aerodynamics X X X X Cadou 674 Aerodynamics of Comp. Fluids X X

Shapiro, Benjamin

54

COPYRIGHT 2003 by ASME AERODYNAMICS OF TIP LEAKAGE FLOWS  

E-Print Network (OSTI)

COPYRIGHT 2003 by ASME 1 AERODYNAMICS OF TIP LEAKAGE FLOWS NEAR PARTIAL SQUEALER RIMS IN AN AXIAL of aerodynamic characteristics of full and partial-length squealer rims in a turbine stage. Full and partial of these "partial squealer tips" and their chordwise position are varied to find an optimal aerodynamic tip

Camci, Cengiz

55

INTRODUCTION 1.1 Aerodynamics of Rotors in Forward Flight  

E-Print Network (OSTI)

1 CHAPTER I INTRODUCTION 1.1 Aerodynamics of Rotors in Forward Flight The prediction of rotor blade aerodynamic loads, especially in forward flight, requires accurate and efficient modeling of several distinct to the nonlinear interaction between the rotor aerodynamics, trim, aeroelasticity and blade dynamics. As stated

56

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

E-Print Network (OSTI)

Journal of Wind Engineering and Industrial Aerodynamics 91 (2003) 1511­1528 New frontiers in aerodynamic tailoring of long span bridges: an advanced analysis framework Xinzhong Chen*, Ahsan Kareem Nat analysis have been made utilizing realistic aerodynamic force modeling for bridges with bluff sections

Chen, Xinzhong

57

Ris-PhD-Report Wind Turbines: Unsteady Aerodynamics and  

E-Print Network (OSTI)

Risø-PhD-Report Wind Turbines: Unsteady Aerodynamics and Inflow Noise Brian Riget Broe Risø-PhD-47 Title: Wind Turbines: Unsteady Aerodynamics and Inflow Noise Division: Wind Energy Division Risø-PhD-47(EN) December 2009 Abstract (max. 2000 char.): Aerodynamical noise from wind turbines due

58

Robust Multi-Objective Optimization in Aerodynamics using MGDA  

E-Print Network (OSTI)

Robust Multi-Objective Optimization in Aerodynamics using MGDA Daigo Maruyama N° 8428-00919215,version1-16Dec2013 #12;Robust Multi-Objective Optimization in Aerodynamics using MGDA Daigo: This study deals with robust design optimization strategies in aerodynamics

Boyer, Edmond

59

AIAA Paper 2001-0870 Re-engineering Aerodynamics Education  

E-Print Network (OSTI)

AIAA Paper 2001-0870 Re-engineering Aerodynamics Education David Darmofal, Earll Murman Aeronautics Paper 2001-0870 Re-engineering Aerodynamics Education David Darmofal* , Earll Murman Massachusetts Institute of Technology Michael Love Lockheed Martin Aeronautics Company Abstract Aerodynamics curriculum

Peraire, Jaime

60

A Genetic Algorithm for Multiobjective Design Optimization in Aerodynamics and  

E-Print Network (OSTI)

A Genetic Algorithm for Multiobjective Design Optimization in Aerodynamics and Electromagnetics R. The objective functions in the optimization problem measure the aerodynamic feasibil­ ity based on the drag been optimized with respect to only one discipline such as aerodynamics or electromagnetics. Although

Coello, Carlos A. Coello

Note: This page contains sample records for the topic "aerodynamic diameter pm" from the National Library of EnergyBeta (NLEBeta).
While these samples are representative of the content of NLEBeta,
they are not comprehensive nor are they the most current set.
We encourage you to perform a real-time search of NLEBeta
to obtain the most current and comprehensive results.


61

Fifty Years of Aerodynamics: Successes, Challenges, and Opportunities  

E-Print Network (OSTI)

Fifty Years of Aerodynamics: Successes, Challenges, and Opportunities T.E. Nelson * D.W. Zingg, Canada. E-mail: tnelson@dehavilland.ca ** Senior Canada Research Chair in Computational Aerodynamics-mail: dwz@oddjob.utias.utoronto.ca Received 22 January 2004. PART I: AIRCRAFT DEVELOPMENT, AERODYNAMIC

Zingg, David W.

62

Single-and Multi-Point Aerodynamic Shape Optimization  

E-Print Network (OSTI)

Single- and Multi-Point Aerodynamic Shape Optimization Using A Parallel Newton-Krylov Approach, Ontario, M3H 5T6, Canada A Newton-Krylov algorithm for aerodynamic shape optimization in three dimensions the capabilities and efficiency of the approach. I. Introduction In the aerodynamic design of aircraft, there have

Zingg, David W.

63

Strategies for Solving High-Fidelity Aerodynamic Shape Optimization Problems  

E-Print Network (OSTI)

Strategies for Solving High-Fidelity Aerodynamic Shape Optimization Problems Zhoujie Lyu Aerodynamic shape optimization based on high-fidelity models is a computational intensive endeavor. The techniques are tested using the Common Research Model wing benchmark defined by the Aerodynamic Design

Papalambros, Panos

64

Aerodynamic Shape Optimization for Aircraft Design Antony Jameson  

E-Print Network (OSTI)

Aerodynamic Shape Optimization for Aircraft Design Antony Jameson Department of Aeronautics September 6-10, 2004 c A. Jameson 2004 Stanford University, Stanford, CA 1/55 Aerodynamic Shape Optimization for Aircraft Design #12;#12; Aerodynamic Design Tradeoffs A good first estimate of performance is provided

Stanford University

65

POLE ASSIGNMENT FOR A VIBRATING SYSTEM WITH AERODYNAMIC EFFECT #  

E-Print Network (OSTI)

POLE ASSIGNMENT FOR A VIBRATING SYSTEM WITH AERODYNAMIC EFFECT # J. N. WANG + , S. H. CHOU # , Y. C­input state feedback control arising from a one­dimensional vibrating system with aerodynamic e real axis. Key words. vibrating system, aerodynamic e#ect, state feedback control, pole assignment AMS

Chou, So-Hsiang

66

Advances in Aerodynamic Shape Optimization Antony Jameson1  

E-Print Network (OSTI)

1 Advances in Aerodynamic Shape Optimization Antony Jameson1 Stanford University, Stanford, CA to aerodynamic design. This shift has been mainly motivated by the availability of high performance comput- ing by J.L. Lions [1]. The method was first used for aerodynamic design by Jameson in 1988 [2, 3]. Since

Jameson, Antony

67

Aerodynamics simulation of operating rooms N. El Gharbi*  

E-Print Network (OSTI)

Aerodynamics simulation of operating rooms N. El Gharbi* A. Benzaoui*R. Bennacer** * Faculty. Keywords: Operating room, aerodynamics simulation, turbulent model, comfort, Airflow, Indoor air quality distribution scheme. To ensure these optimal conditions, a study of the aerodynamics flow in a conditioned

Paris-Sud XI, Université de

68

Optimum Aerodynamic Design using the Navier--Stokes Equations  

E-Print Network (OSTI)

Optimum Aerodynamic Design using the Navier--Stokes Equations A. JAMESON \\Lambda ; N.A. PIERCE y factors such as aerodynamic effi­ ciency, structural weight, stability and control, and the volume the disciplines. The development of accurate and efficient methods for aerodynamic shape optimization represents

Pierce, Niles A.

69

POLE ASSIGNMENT FOR A VIBRATING SYSTEM WITH AERODYNAMIC EFFECT  

E-Print Network (OSTI)

POLE ASSIGNMENT FOR A VIBRATING SYSTEM WITH AERODYNAMIC EFFECT J. N. WANG, S. H. CHOU, Y. C. CHEN feedback control arising from a one-dimensional vibrating system with aerodynamic effect. On the practical real axis. Key words. vibrating system, aerodynamic effect, state feedback control, pole assignment AMS

Lin, Wen-Wei

70

On Aerodynamic Optimization Under a Range of Operating Conditions  

E-Print Network (OSTI)

On Aerodynamic Optimization Under a Range of Operating Conditions David W. Zingg, and Samy Elias In aerodynamic design, good performance is generally required under a range of oper- ating conditions, including aerodynamic shape optimization.1­6 The designer specifies an objective, operating conditions, constraints

Zingg, David W.

71

Unsteady aerodynamic models for agile flight at low Reynolds numbers  

E-Print Network (OSTI)

Unsteady aerodynamic models for agile flight at low Reynolds numbers Steven L. Brunton , Clarence W for the unsteady aerodynamic forces on a small wing in response to agile maneuvers and gusts. In a previous study, it was shown that Theodorsen's and Wagner's unsteady aerodynamic models agree with force data from DNS

Rowley, Clarence W.

72

An Evolutionary Geometry Parametrization for Aerodynamic Shape Optimization  

E-Print Network (OSTI)

An Evolutionary Geometry Parametrization for Aerodynamic Shape Optimization Xiaocong Han and David, M3H 5T6, Canada An evolutionary geometry parametrization is presented for aerodynamic shape optimiza, unconventional aerodynamic configurations. Based on improvements in computational fluid dynamics (CFD) and high

Zingg, David W.

73

A Pilot Project in Preparation of an Aerodynamic Optimization Workshop  

E-Print Network (OSTI)

A Pilot Project in Preparation of an Aerodynamic Optimization Workshop with Lessons Learned John C-scale Aerodynamic Optimization Workshop. Three independent optimization efforts were conducted concurrently, each in the preparation of a possible future workshop on aerodynamic shape optimization. 1.0 Introduction During AIAA

Jameson, Antony

74

Aerodynamic Force Modeling for Unsteady Wing Ryan Jantzen  

E-Print Network (OSTI)

Aerodynamic Force Modeling for Unsteady Wing Maneuvers Ryan Jantzen and Kunihiko Taira Florida, Wright-Patterson Air Force Base, OH We report on the development of an aerodynamic force model for a flat focus is placed on examining the influence of large-amplitude wing motion on the unsteady aerodynamics

75

Ris-R-1543(EN) Aerodynamic investigation of Winglets on  

E-Print Network (OSTI)

Risø-R-1543(EN) Aerodynamic investigation of Winglets on Wind Turbine Blades using CFD Jeppe Johansen and Niels N. Sørensen Title: Aerodynamic investigation of Winglets on Wind Turbine Blades using of the aerodynamics around a wind turbine blade with a winglet using Computational Fluid Dynamics, CFD. Five winglets

76

Error estimation and adaptive mesh refinement for aerodynamic flows  

E-Print Network (OSTI)

Error estimation and adaptive mesh refinement for aerodynamic flows Ralf Hartmann, Joachim Held-oriented mesh refinement for single and multiple aerodynamic force coefficients as well as residual-based mesh refinement applied to various three-dimensional lam- inar and turbulent aerodynamic test cases defined

Hartmann, Ralf

77

Managing Approximate Models in Evolutionary Aerodynamic Design Optimization  

E-Print Network (OSTI)

Managing Approximate Models in Evolutionary Aerodynamic Design Optimization Yaochu Jin yaochu jin­ mization problems that are discontinuous, multi­modal and multi­objective [1, 2]. Aerodynamic structural to high complexity of the aerodynamic analysis and large number of evaluations needed in the evolutionary

Coello, Carlos A. Coello

78

Optimizing the Aerodynamic Efficiency of IM Freight Trains  

E-Print Network (OSTI)

Optimizing the Aerodynamic Efficiency of IM Freight Trains Yung-Cheng Lai University of Illinois aerodynamic penalties and fuel consumption than general trains IM trains suffer from their equipment design and loading pattern These large gaps directly affect the aerodynamic drag of the train. This effect is greater

Barkan, Christopher P.L.

79

THE VELOCITY DEPENDENCE OF AERODYNAMIC DRAG: A PRIMER FOR MATHEMATICIANS  

E-Print Network (OSTI)

THE VELOCITY DEPENDENCE OF AERODYNAMIC DRAG: A PRIMER FOR MATHEMATICIANS LYLE N. LONG and HOWARD­entry of the space shuttle into the earth's atmosphere. Dimensional analysis is an important tool in aerodynamics­T E X 1 #12; For detailed information on the aerodynamics and fluid mechanics pertinent to this paper

80

RESEARCH ARTICLE Aerodynamic and functional consequences of wing compliance  

E-Print Network (OSTI)

RESEARCH ARTICLE Aerodynamic and functional consequences of wing compliance Andrew M. Mountcastle Ã?, the instantaneous shape of an insect wing is dictated by the interaction of aerodynamic forces with the inertial rever- sals--loads that well exceed the mean aerodynamic force. Although wing compliance has been

Daniel, Tom

Note: This page contains sample records for the topic "aerodynamic diameter pm" from the National Library of EnergyBeta (NLEBeta).
While these samples are representative of the content of NLEBeta,
they are not comprehensive nor are they the most current set.
We encourage you to perform a real-time search of NLEBeta
to obtain the most current and comprehensive results.


81

Numerical Aerodynamic Optimization Incorporating Laminar-Turbulent Transition Prediction  

E-Print Network (OSTI)

Numerical Aerodynamic Optimization Incorporating Laminar-Turbulent Transition Prediction J. Driver-dimensional Newton­Krylov aerodynamic shape optimization algorithm is applied to several optimization problems a striking demonstration of the capability of the Newton­ Krylov aerodynamic optimization algorithm to design

Zingg, David W.

82

Optimizing the aerodynamic efficiency of intermodal freight trains  

E-Print Network (OSTI)

Optimizing the aerodynamic efficiency of intermodal freight trains Yung-Cheng Lai a,*, Christopher form 24 April 2007; accepted 17 May 2007 Abstract We develop an aerodynamic loading assignment model fuel-efficient trains. This is the first use of optimization modeling to address the aerodynamics

Barkan, Christopher P.L.

83

Aerodynamic beam generator for large particles  

DOE Patents (OSTI)

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.

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)

2002-01-01T23:59:59.000Z

84

Computerized method and system for designing an aerodynamic focusing lens stack  

DOE Patents (OSTI)

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.

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)

2011-11-22T23:59:59.000Z

85

Tightening procedures for large diameter anchor bolts  

E-Print Network (OSTI)

Standards for tightening procedures for large diameter anchor bolts are proposed. These bolts, 38 mm (I 1/2 in.) in diameter or greater, are widely used in highway appurtenance. In current practices, the contractor is left to his or her own...

Abraham, Ryan Charles

2012-06-07T23:59:59.000Z

86

Aerodynamic characteristics of a feathered dinosaur measured using physical models. Effects of form on static stability and control effectiveness  

E-Print Network (OSTI)

McCay MG (2001) Aerodynamic stability and maneuverability ofrain forest canopy: the aerodynamic environment of gliding2011) Measurement of the aerodynamic stability and control

Evangelista, Dennis

2013-01-01T23:59:59.000Z

87

Aerodynamics of a rigid curved kite wing  

E-Print Network (OSTI)

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...

Maneia, Gianmauro; Tordella, Daniela; Iovieno, Michele

2013-01-01T23:59:59.000Z

88

Inertial and Aerodynamic Tail Steering of a Meso-scale Legged Robot  

E-Print Network (OSTI)

Legged Robots Use of Aerodynamics 2.5 Overview of previousare the use of passive aerodynamics in running robots. Fi-the first use of passive aerodynamics to induce a turn in a

Kohut, Nicholas Jospeh

2013-01-01T23:59:59.000Z

89

Transient Aerodynamic Effects on a Four-Car Platoon During Passing Maneuvers: Data Summary  

E-Print Network (OSTI)

B. Marcu, F. Browand, ”The Aerodynamic Forces on Misalignedof the Transient Aerodynamic Effects on a Four-Car PlatoonBERKELEY Transient Aerodynamic Effects on a Four-Car Platoon

Tsuei, L.; Hedrick, J. K.; Savas, O.

1999-01-01T23:59:59.000Z

90

Precision wire feeder for small diameter wire  

SciTech Connect

This invention is comprised of a device for feeding small diameter wire having a diameter less than .04 mm (16 mil) to a welding station which 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 fig.

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

1990-12-31T23:59:59.000Z

91

E-Print Network 3.0 - aerodynamic shape optimization Sample Search...  

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Search Powered by Explorit Topic List Advanced Search Sample search results for: aerodynamic shape optimization Page: << < 1 2 3 4 5 > >> 1 Aerodynamic shape and planform...

92

E-Print Network 3.0 - aerodynamic particle sizer Sample Search...  

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Search Powered by Explorit Topic List Advanced Search Sample search results for: aerodynamic particle sizer Page: << < 1 2 3 4 5 > >> 1 Aerodynamic Particle Sizer Spectrometer...

93

E-Print Network 3.0 - aerodynamics Sample Search Results  

NLE Websites -- All DOE Office Websites (Extended Search)

Airfoil Summary: Design Ahmed Abdelwahab Manager of Turbomachinery Aerodynamics Praxair Inc., Global Supply System... engineer to aerodynamic designer to lead aerodynamicist...

94

E-Print Network 3.0 - aerodynamic design features Sample Search...  

NLE Websites -- All DOE Office Websites (Extended Search)

Airfoil Summary: Design Ahmed Abdelwahab Manager of Turbomachinery Aerodynamics Praxair Inc., Global Supply System... engineer to aerodynamic designer to lead aerodynamicist...

95

E-Print Network 3.0 - aerodynamic stability Sample Search Results  

NLE Websites -- All DOE Office Websites (Extended Search)

of the aerodynamic resistance S. Liu, D. Mao, and L. Lu State key Laboratory of Remote Sensing Science, School... -705, 2006 Measurement and estimation of the aerodynamic...

96

E-Print Network 3.0 - aiaa aerodynamic measurement Sample Search...  

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of Aerospace and Ocean Engineering, Virginia Tech Collection: Engineering 24 Airfoil Ice-Accretion Aerodynamics Simulation and A. Broeren Summary: is required for aerodynamic...

97

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

SciTech Connect

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.

Schreck, S.; Robinson, M.

2007-08-01T23:59:59.000Z

98

Aerodynamic Focusing Of High-Density Aerosols  

SciTech Connect

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.

Ruiz, D. E.; Fisch, Nathaniel

2014-02-24T23:59:59.000Z

99

Experimental aerodynamics research on a hypersonic vehicle  

SciTech Connect

Aerodynamic force and moment measurements and flow visualization results are presented for a hypersonic vehicle configuration at Mach 8. The basic vehicle configuration is a spherically blunted 10[degree] half-angle cone with a slice parallel with the axis of the vehicle. On the slice portion of the vehicle, a flap could be attached so that deflection angles of 10[degree], 20[degree] and 30[degree] could be obtained. All of the experimental results were obtained in the Sandia Mach 8 hypersonic wind tunnel for laminar boundary layer conditions. Flow visualization results include shear stress sensitive liquid crystal photographs, surface streak flow photographs (using liquid crystals), and spark schlieren photographs and video. The liquid crystals were used as an aid in verifying that a laminar boundary layer existed over the entire body. The surface flow photo-graphs show attached and separated flow on both the leeside of the vehicle and near the flap. A detailed uncertainty analysis was conducted to estimate the contributors to body force and moment measurement uncertainty. Comparisons are made with computational results to evaluate both the experimental and numerical results. This extensive set of high-quality experimental force and moment measurements is recommended for use in the calibration and validation of relevant computational aerodynamics codes.

Oberkampf, W.L.; Aeschliman, D.P.; Tate, R.E.; Henfling, J.F.

1993-04-01T23:59:59.000Z

100

Experimental aerodynamics research on a hypersonic vehicle  

SciTech Connect

Aerodynamic force and moment measurements and flow visualization results are presented for a hypersonic vehicle configuration at Mach 8. The basic vehicle configuration is a spherically blunted 10{degree} half-angle cone with a slice parallel with the axis of the vehicle. On the slice portion of the vehicle, a flap could be attached so that deflection angles of 10{degree}, 20{degree} and 30{degree} could be obtained. All of the experimental results were obtained in the Sandia Mach 8 hypersonic wind tunnel for laminar boundary layer conditions. Flow visualization results include shear stress sensitive liquid crystal photographs, surface streak flow photographs (using liquid crystals), and spark schlieren photographs and video. The liquid crystals were used as an aid in verifying that a laminar boundary layer existed over the entire body. The surface flow photo-graphs show attached and separated flow on both the leeside of the vehicle and near the flap. A detailed uncertainty analysis was conducted to estimate the contributors to body force and moment measurement uncertainty. Comparisons are made with computational results to evaluate both the experimental and numerical results. This extensive set of high-quality experimental force and moment measurements is recommended for use in the calibration and validation of relevant computational aerodynamics codes.

Oberkampf, W.L.; Aeschliman, D.P.; Tate, R.E.; Henfling, J.F.

1993-04-01T23:59:59.000Z

Note: This page contains sample records for the topic "aerodynamic diameter pm" from the National Library of EnergyBeta (NLEBeta).
While these samples are representative of the content of NLEBeta,
they are not comprehensive nor are they the most current set.
We encourage you to perform a real-time search of NLEBeta
to obtain the most current and comprehensive results.


101

Lasing in microdisks of ultrasmall diameter  

SciTech Connect

It is demonstrated by calculations and experimental results that room-temperature lasing can be obtained at the ground-state optical transition of InAs/InGaAs/GaAs quantum dots in optical microcavities with a record-small diameter of 1.5 ?m. In 1-?m cavities, lasing occurs at the wavelength of one of the whispering-gallery modes within the band corresponding to the first excited-state optical transition.

Zhukov, A. E., E-mail: zhukale@gmail.com; Kryzhanovskaya, N. V.; Maximov, M. V.; Lipovskii, A. A.; Savelyev, A. V.; Bogdanov, A. A.; Shostak, I. I.; Moiseev, E. I.; Karpov, D. V. [St. Petersburg Academic University—Nanotechnology Research and Education Center, Russian Academy of Sciences (Russian Federation); Laukkanen, J. [University of Eastern Finland, Institute of Photonics (Finland); Tommila, J. [Tampere University of Technology, Optoelectronics Research Centre (Finland)

2014-12-15T23:59:59.000Z

102

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

NLE Websites -- All DOE Office Websites (Extended Search)

Diameter-Refined Metallic Carbon Nanotubes as Optically Tunable Transparent Conductors Home > Research > ANSER Research Highlights > Diameter-Refined Metallic Carbon Nanotubes as...

103

Modeling FullEnvelope Aerodynamics of Small UAVs in RealTime Prof. Michael Selig  

E-Print Network (OSTI)

D M E S S Modeling FullEnvelope Aerodynamics of Small UAVs in RealTime Prof. Michael Selig Applied Aerodynamics Group and Subsonic Aerodynamics Research Lab Department of Aerospace Engineering will focus on the development of a full six degreeoffreedom aerodynamics modeling environment for small UAVs

Barthelat, Francois

104

E-Print Network 3.0 - aerodynamic drag presentation Sample Search...  

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presentation Search Powered by Explorit Topic List Advanced Search Sample search results for: aerodynamic drag presentation...

105

Aerodynamic-Structural Design Studies of Low-Sweep Transonic Wings  

E-Print Network (OSTI)

Aerodynamic-Structural Design Studies of Low-Sweep Transonic Wings Antony Jameson Department level. High-fidelity aerodynamic and aerodynamic-structural optimizations are performed on a set to significantly reduce wing sweep without incurring either aerodynamic or structural penalties, especially for M

Jameson, Antony

106

E-Print Network 3.0 - aerodynamic drag presentations Sample Search...  

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presentations Search Powered by Explorit Topic List Advanced Search Sample search results for: aerodynamic drag presentations...

107

Unsteady aerodynamic analysis of subsonic oscillating cascade  

SciTech Connect

This paper describes the development of the source-doublet-based potential paneling method for oscillating cascade unsteady aerodynamic load predictions. By using the integral influence coefficient method and by using the interblade phase angles, the unsteady loads on an oscillating cascade can be accurately predicted at a minimum cost. As the grids are placed only on the blade surfaces, the blades are allowed to vibrate without grid deformation problems. Four notable subsonic oscillating cascade test cases that cover most important parameters, e.g., blade geometry, interblade phase angle, flow coefficient, flow speed, frequency, etc., are studied in this paper. The agreement between the present solutions and other numerical/experimental results demonstrates the robustness of the present model. Applicability of the method for realistic compressible flow cascades is also discussed.

Chen, S.H.; Eastland, A.H.; Jackson, E.D. (Rockwell International Corp., Canoga Park, CA (United States). Rocketdyne Div.)

1994-07-01T23:59:59.000Z

108

CFD calculations of S809 aerodynamic characteristics  

SciTech Connect

Steady-state, two-dimensional CFD calculations were made for the S809 laminar-flow, wind-turbine airfoil using the commercial code CFD-ACE. Comparisons of the computed pressure and aerodynamic coefficients were made with wind tunnel data from the Delft University 1.8 m x 1.25 m low-turbulence wind tunnel. 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-{epsilon} model, is not appropriate at angles of attack with flow separation.

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

1997-01-01T23:59:59.000Z

109

Hypersonic Arbitrary-Body Aerodynamics (HABA) for conceptual design  

SciTech Connect

The Hypersonic Arbitrary-Body Aerodynamics (HABA) computer program predicts static and dynamic aerodynamic derivatives at hypersonic speeds for any vehicle geometry. It is intended to be used during conceptual design studies where fast computational speed is required. It uses the same geometry and hypersonic aerodynamic methods as the Mark IV Supersonic/Hypersonic Arbitrary-Body Program (SHABP) developed under sponsorship of the Air Force Flight Dynamics Laboratory; however, the input and output formats have been improved to make it easier to use. This program is available as part of the Department 9140 CAE software.

Salguero, D.E.

1990-03-15T23:59:59.000Z

110

Thread gauge for measuring thread pitch diameters  

DOE Patents (OSTI)

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.

Brewster, A.L.

1985-11-19T23:59:59.000Z

111

Thread gauge for measuring thread pitch diameters  

DOE Patents (OSTI)

A thread gauge which attaches to a vernier caliper to measure the thread pitch diameter of both externally threaded and internally threaded parts. 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.

Brewster, Albert L. (R.R. 2, Box 190A, Pleasant Hill, MO 64080)

1985-01-01T23:59:59.000Z

112

Applications of Proper Orthogonal Decomposition for Inviscid Transonic Aerodynamics  

E-Print Network (OSTI)

Two extensions to the proper orthogonal decomposition (POD) technique are considered for steady transonic aerodynamic applications. The first is to couple the POD approach with a cubic spline interpolation procedure in ...

Tan, Bui-Thanh

113

Mathematical simulation of wind-wheel aerodynamic performances  

Science Journals Connector (OSTI)

A mathematical model of wind-wheel aerodynamic performances for a wind-power plant is developed. This model makes it possible to both calculate wind turbine performance and recover it for any blade pitch angles.

P. S. Tsgoev

2009-11-01T23:59:59.000Z

114

Flow visualization and analysis of aerodynamically detuned supersonic rotors  

Science Journals Connector (OSTI)

The effect of aerodynamic detuning on the supersonic steady and unsteady blade passage flow field is experimentally investigated on a free surface water table by means of color Schlieren and shadowgraph flow v...

C. S. Farmer; S. Fleeter

1988-01-01T23:59:59.000Z

115

Structural and Aerodynamic Interaction Computational Tool for Highly Reconfigurable Wings  

E-Print Network (OSTI)

of the aerospace industry, and a reconfigurable wing is a significant element of a morphing aircraft. This thesis develops two tools for analyzing wing configurations with multiple geometric degrees-of-freedom: the structural tool and the aerodynamic and structural...

Eisenbeis, Brian Joseph

2011-10-21T23:59:59.000Z

116

Aerodynamic Design for Swept-wing Laminar Flow  

E-Print Network (OSTI)

This work describes and compares processes for swept-wing laminar flow control (SWLFC) aerody-namic design. It focuses on results obtained during the preliminary outer-mold-line (OML) design of the Subsonic Aircraft Roughness Glove Experiment...

Belisle, Michael Joseph

2013-11-08T23:59:59.000Z

117

American Institute of Aeronautics and Astronautics AERODYNAMIC OPTIMIZATION FOR FREIGHT  

E-Print Network (OSTI)

American Institute of Aeronautics and Astronautics 1 AERODYNAMIC OPTIMIZATION FOR FREIGHT TRUCKS and Astronautics 2 controls,4 , flight trajectories,5 wings and airfoils,6,7,9,10 inlets,14 rockets,16,19 missiles

Roy, Chris

118

Title: Aerodynamic and Scalar Roughness over Snow and Sea Ice In Monin-Obukhov similarity theory, the aerodynamic roughness, z0, is the artificial height  

E-Print Network (OSTI)

Title: Aerodynamic and Scalar Roughness over Snow and Sea Ice Abstract: In Monin-Obukhov similarity theory, the aerodynamic roughness, z0, is the artificial height above the surface at which the wind speed the theory and measurement of the aerodynamic and scalar roughness lengths over snow and sea ice. The data

119

Search for $\\delta^{\\pm\\pm}$ with new decay patterns at LHC  

E-Print Network (OSTI)

A study of searching for doubly charged Higgs $(\\delta^{\\pm \\pm})$ is performed in two-Higgs-doublet extension of the conventional type-II seesaw model. We find that a fantastic mixing effect between singly charged Higgs of Higgs doublet and of triplet is arisen from the scalar potential. The mixing leads to following intriguing phenomena: (a) the mass splittings in triplet particles are magnified, (b) QCD processes dominate the production of $\\delta^{\\pm \\pm}$, and (c) new predominant decay channels of $\\delta^{\\pm \\pm}$ are $\\delta^{\\pm \\pm} \\to W^{\\pm^{[*]}} H^{\\pm^{(*)}}_{1(2)}$, but not $\\delta^{\\pm} \\to (\\ell^\\pm \\ell^\\pm, W^\\pm W^\\pm)$ which are usually discussed in the literature. With luminosity of 40 fb$^{-1}$ and collision energy of 13 TeV, we demonstrate that $\\delta^{\\pm \\pm}$ with mass below $330$ GeV could be observed at the $5\\sigma$ level. Moreover, when the luminosity approaches to 300 fb$^{-1}$, the observed mass of $\\delta^{\\pm \\pm}$ could reach up to 450 GeV.

Chen, Chuan-Hung

2014-01-01T23:59:59.000Z

120

Aerodynamic characteristics of a feathered dinosaur measured using physical models. Effects of form on static stability and control effectiveness  

E-Print Network (OSTI)

2007) Fundamentals of Aerodynamics. New York, NY: McGraw-31. McCormick BW (1995) Aerodynamics, Aeronautics and FlightA computational study of the aerodynamics and forewing-

Evangelista, Dennis

2013-01-01T23:59:59.000Z

Note: This page contains sample records for the topic "aerodynamic diameter pm" from the National Library of EnergyBeta (NLEBeta).
While these samples are representative of the content of NLEBeta,
they are not comprehensive nor are they the most current set.
We encourage you to perform a real-time search of NLEBeta
to obtain the most current and comprehensive results.


121

Aerodynamic Analysis of Intermodal Freight Trains Using Machine Vision World Congress on Railway Research, May 22-26, 2011  

E-Print Network (OSTI)

Aerodynamic Analysis of Intermodal Freight Trains Using Machine Vision 9 th World Congress. However, intermodal trains use rolling stock that generates significantly greater aerodynamic drag increases annual operating expenditures. There are opportunities to improve intermodal train aerodynamics

Illinois at Urbana-Champaign, University of

122

ccsd00003793, Room temperature Peierls distortion in small diameter nanotubes  

E-Print Network (OSTI)

nanotubes D. Conn#19;etable, 1 G.-M. Rignanese, 2, 3 J.-C. Charlier, 2, 3 and X. Blase 1 1 Laboratoire de structure and electron-phonon coupling in small 4- #23; A diameter nanotubes. We show that both the C(5 the diameter decreases. These results question the origin of superconductivity in small diameter nanotubes

123

WING TIP ANATOMY AND AERODYNAMICS IN FLYING National Museum of Natural History, Department of Vertebrate Zoology,  

E-Print Network (OSTI)

WING TIP ANATOMY AND AERODYNAMICS IN FLYING SQUIRRELS National Museum of Natural History aerodynamically sophisticat- back into a curve by the tibiocarpalis mus- ed. They are able to modify shape

Mathis, Wayne N.

124

Aeolian sediment transport pathways and aerodynamics at troughs Mary C. Bourke1  

E-Print Network (OSTI)

Aeolian sediment transport pathways and aerodynamics at troughs on Mars Mary C. Bourke1 School pathways and aerodynamics at troughs on Mars, J. Geophys. Res., 109, E07005, doi:10.1029/2003JE002155. 1

Bourke, Mary C.

125

Aerodynamic Focusing of High-Density Aerosols D.E. Ruiza,  

E-Print Network (OSTI)

Aerodynamic Focusing of High-Density Aerosols D.E. Ruiza, , L. Gundersona , M.J. Haya , E. Merinob-density aerosol focusing for 1µm silica spheres. Preliminary results recover previous findings on aerodynamic

126

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

E-Print Network (OSTI)

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...

Suryanarayanan, Arun

2010-07-14T23:59:59.000Z

127

Unsteady aerodynamic forces on small-scale wings: experiments, simulations and models  

E-Print Network (OSTI)

Unsteady aerodynamic forces on small-scale wings: experiments, simulations and models Steven L for the unsteady aerodynamics. It is possible to obtain reduced order models by projective methods such as balanced

Dabiri, John O.

128

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

E-Print Network (OSTI)

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 ...

Cote, Mark (Mark Brian)

2007-01-01T23:59:59.000Z

129

E-Print Network 3.0 - aerodynamic test facilities Sample Search...  

NLE Websites -- All DOE Office Websites (Extended Search)

test facilities Search Powered by Explorit Topic List Advanced Search Sample search results for: aerodynamic test facilities Page: << < 1 2 3 4 5 > >> 1 A Tour of the Aerodynamic...

130

Aerodynamic Effects in Weakly Ionized Gas: Phenomenology and Applications  

SciTech Connect

Aerodynamic effects in ionized gases, often neglected phenomena, have been subject of a renewed interest in recent years. After a brief historical account, we discuss a selected number of effects and unresolved problems that appear to be relevant in both aeronautic and propulsion applications in subsonic, supersonic, and hypersonic flow. Interaction between acoustic shock waves and weakly ionized gas is manifested either as plasma-induced shock wave dispersion and acceleration or as shock-wave induced double electric layer in the plasma, followed by the localized increase of the average electron energy and density, as well as enhancement of optical emission. We describe the phenomenology of these effects and discuss several experiments that still do not have an adequate interpretation. Critical for application of aerodynamic effects is the energy deposition into the flow. We classify and discuss some proposed wall-free generation schemes with respect to the efficiency of energy deposition and overall generation of the aerodynamic body force.

Popovic, S.; Vuskovic, L. [Department of Physics, Old Dominion University, Norfolk, Virginia (United States)

2006-12-01T23:59:59.000Z

131

Joint computational and experimental aerodynamics research on a hypersonic vehicle  

SciTech Connect

A closely coupled computational and experimental aerodynamics research program was conducted on a hypersonic vehicle configuration at Mach 8. Aerodynamic force and moment measurements and flow visualization results were obtained in the Sandia National Laboratories hypersonic wind tunnel for laminar boundary layer conditions. Parabolized and iterative Navier-Stokes simulations were used to predict flow fields and forces and moments on the hypersonic configuration. The basic vehicle configuration is a spherically blunted 10{degrees} cone with a slice parallel with the axis of the vehicle. On the slice portion of the vehicle, a flap can be attached so that deflection angles of 10{degrees}, 20{degrees}, and 30{degrees} can be obtained. Comparisons are made between experimental and computational results to evaluate quality of each and to identify areas where improvements are needed. This extensive set of high-quality experimental force and moment measurements is recommended for use in the calibration and validation of computational aerodynamics codes. 22 refs.

Oberkampf, W.L.; Aeschliman, D.P.; Walker, M.M.

1992-01-01T23:59:59.000Z

132

Validation Testing for the PM-PEMS Measurement Allowance Program  

E-Print Network (OSTI)

propane verifications are required to verify PM measurementsverification process for its PM mass sensitivity measurementtheir PM measurement system. The PEMS3 verification is based

Johnson, K; Durbin, T; Jung, H; Cocker III, D R; Khan, M Y

2010-01-01T23:59:59.000Z

133

Nuclear Orientation of Pm143  

Science Journals Connector (OSTI)

Promethium-143 has been oriented in a crystal of neodymium ethylsulfate. The angular distribution of the 740-kev ? ray was found to be W(?)=1-(0.065±0.006)P2(cos?) at 0.02°K. Values for the mixing ratio, ?, of the 740-kev ? ray of Nd143 were obtained as a function of the magnetic moment of the ground state of Pm143. The spin of the excited state of Nd143 was assigned as 92-. An absolute lower limit of |?|>1.0 was set on the magnetic moment of Pm143. The mixing ratio of the ? ray of Nd143 was found to lie in the range 0.23

C. A. Lovejoy, J. O. Rasmussen, and D. A. Shirley

1961-08-01T23:59:59.000Z

134

Investigation of aerodynamic braking devices for wind turbine applications  

SciTech Connect

This report documents the selection and preliminary design of a new aerodynamic braking system for use on the stall-regulated AWT-26/27 wind turbines. The goal was to identify and design a configuration that offered improvements over the existing tip brake used by Advanced Wind Turbines, Inc. (AWT). Although the design objectives and approach of this report are specific to aerodynamic braking of AWT-26/27 turbines, many of the issues addressed in this work are applicable to a wider class of turbines. The performance trends and design choices presented in this report should be of general use to wind turbine designers who are considering alternative aerodynamic braking methods. A literature search was combined with preliminary work on device sizing, loads and mechanical design. Candidate configurations were assessed on their potential for benefits in the areas of cost, weight, aerodynamic noise, reliability and performance under icing conditions. As a result, two configurations were identified for further study: the {open_quotes}spoiler-flap{close_quotes} and the {open_quotes}flip-tip.{close_quotes} Wind tunnel experiments were conducted at Wichita State University to evaluate the performance of the candidate aerodynamic brakes on an airfoil section representative of the AWT-26/27 blades. The wind tunnel data were used to predict the braking effectiveness and deployment characteristics of the candidate devices for a wide range of design parameters. The evaluation was iterative, with mechanical design and structural analysis being conducted in parallel with the braking performance studies. The preliminary estimate of the spoiler-flap system cost was $150 less than the production AWT-26/27 tip vanes. This represents a reduction of approximately 5 % in the cost of the aerodynamic braking system. In view of the preliminary nature of the design, it would be prudent to plan for contingencies in both cost and weight.

Griffin, D.A. [R. Lynette & Associates, Seattle, WA (United States)

1997-04-01T23:59:59.000Z

135

E-Print Network 3.0 - airfoil aerodynamic performance Sample...  

NLE Websites -- All DOE Office Websites (Extended Search)

Compressors... Design Ahmed Abdelwahab Manager of Turbomachinery Aerodynamics Praxair Inc., Global Supply System... -dimensional airfoil diffuser designs is presented....

136

Reentry aerodynamic disruption analysis of thermionic reactor-thermo-converter TOPAZ-2  

SciTech Connect

This paper presents preliminary results of analysis for the TOPAZ-2 thermionic converter-reactor aerodynamic disruption during reentry.

Grinberg, E.I.; Nikolaev, V.S. (Scientific Production Association Krasnaya Zvezda'', Moscow 115230 (Russian Federation)); Usov, V.A. (RRC Kurchatov Institute'', Moscow 123182 (Russian Federation)); Gafarov, A.A. (Research Institute of Thermal Processes, Moscow (Russian Federation))

1993-01-15T23:59:59.000Z

137

PM  

NLE Websites -- All DOE Office Websites (Extended Search)

RD RD Start Finish PBS030_1.4.1 ENVIRONMENTAL RESTORATION PROJECT - VL-NV-00 2807 10-02-06 A 07-03-18 PBS030_1.4.1.1 SOILS 2807 10-01-07 07-03-18 PBS030_1.4.1.1.03 CAU 413 CLEAN SLATE II PLUTONIUM DISPERSION (TTR) 2807 10-01-07 07-03-18 PBS030_1.4.1.1.03.09 PROJECT MANAGEMENT 2807 10-01-07 07-03-18 Project Management 2807 10-01-07* 07-03-18 PBS030_1.4.1.1.06 CAU 366 AREA 11 PLUTONIUM VALLEY UNIT SAFETY SHO 476 12-01-10 09-26-12 PBS030_1.4.1.1.06.01 CORRECTIVE ACTION INVESTIGATION PLAN (CAIP) 185 12-01-10 08-16-11 Corrective Action Investigation Plan 185 12-01-10* 08-16-11 PBS030_1.4.1.1.06.02 CADD/CR 426 02-09-11 09-26-12 CADD/CR 426 02-09-11 09-26-12 CADD/CR to State 0 09-26-12 PBS030_1.4.1.1.07 CAU 365 AREA 5 GMX UNIT SAFETY SHOTS 526 11-02-09 11-07-11 PBS030_1.4.1.1.07.01 CORRECTIVE ACTION INVESTIGATION PLAN (CAIP)

138

PM  

NLE Websites -- All DOE Office Websites (Extended Search)

of an assessment of needs and program reqs 42015 11416 8948 707,086 1.7.1.06 Conduct of Operations Program 1.7.1.06 Conduct of Operations Program 5114 A 11216...

139

ACARS Aerodynamic (Research Incorporated) Communication and Recording System  

NLE Websites -- All DOE Office Websites (Extended Search)

ix ix Acrononyms and Abbreviations Acronyms and Abbreviations ACARS Aerodynamic (Research Incorporated) Communication and Recording System ACSYS Arctic Climate System Study AER Atmospheric Environmental Research, Inc. AERI Atmospheric Emitted Radiance Interferometer AFOSR Air Force Office of Scientific Research AGARD Advisory Group for Aerospace Research and Development ALFA AER Local Forecast and Assimilation (model) AMIP Atmospheric Model Intercomparison Project ARCS Atmosphere Radiation and Cloud Stations ARCSS Arctic System Science (NSF) ARCSYM Arctic Regional Climate System Model ARINC Aerodynamic Research Incorporated Communication ARM Atmospheric Radiation Measurement program AS anvil stratus ASTER Atmosphere-Surface Turbulent Exchange Research ASTEX Altantic Stratocumulus Transition EXperiment

140

Progress in Aerospace Sciences 39 (2003) 185248 The unsteady aerodynamics of slender wings and aircraft  

E-Print Network (OSTI)

Progress in Aerospace Sciences 39 (2003) 185­248 The unsteady aerodynamics of slender wings nonlinearities and flow field time lags. The aerodynamic and the vortical flow structure over simple delta wings of leading-edge vortices and their influence on delta wing aerodynamics for stationary models is presented

Nelson, Robert C.

Note: This page contains sample records for the topic "aerodynamic diameter pm" from the National Library of EnergyBeta (NLEBeta).
While these samples are representative of the content of NLEBeta,
they are not comprehensive nor are they the most current set.
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141

International Symposium of Applied Aerodynamics Lille, 24-25-26 March 2014  

E-Print Network (OSTI)

49th International Symposium of Applied Aerodynamics Lille, 24-25-26 March 2014 FP05-2014-paquet Formulation of Aerodynamic Forces on Helicopters in Non Uniform Flow with Scale Model Tests : Ground Effects. The number of state variables influencing the aerodynamic forces are too numerous so it is not possible

142

The Effects of Turbulence on the Aerodynamics of Oscillating Fred L. Haan, Jr a  

E-Print Network (OSTI)

The Effects of Turbulence on the Aerodynamics of Oscillating Prisms Fred L. Haan, Jr a , Ahsan ABSTRACT: This experimental study, focusing on the effects of turbulence on long-span bridge aerodynamics and the spanwise correlation of the overall aerodynamic lift and moment. This exami- nation was conducted

Kareem, Ahsan

143

International Symposium of Applied Aerodynamics Lille, 24-25-26 March 2014  

E-Print Network (OSTI)

49th International Symposium of Applied Aerodynamics Lille, 24-25-26 March 2014 FP04-2014-arntz Numerical Airframe Aerodynamic Performance Prediction: An Exergy Point of View Aurélien Arntz, Olivier.arntz@onera.fr, olivier.atinault@onera.fr, daniel.destarac@onera.fr ABSTRACT The prediction of the aerodynamic performance

144

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

E-Print Network (OSTI)

Courses for Breadth Requirement of Aerospace Engineering M.S. Degree Program Aerodynamics, Fluid Mechanics, Combustion and Propulsion (AFMCP) AE 410/CSE 461: Computational Aerodynamics AE 412/ME 411: Viscous Flow & Heat Transfer AE 416: Applied Aerodynamics AE 419: Aircraft Flight Mechanics AE 433

Gilbert, Matthew

145

25th AIAA Applied Aerodynamics Conference June 2528, 2007/Miami, FL  

E-Print Network (OSTI)

25th AIAA Applied Aerodynamics Conference June 25­28, 2007/Miami, FL Validation Study of Aerodynamic Analysis Tools for Design Optimization of Helicopter Rotors Seongim Choi , Juan J. Alonso , Edwin current aerodynamic analysis tools in predicting the unsteady flow field generated by helicopter rotors

Alonso, Juan J.

146

International Symposium of Applied Aerodynamics Lille, 24-25-26 March 2014  

E-Print Network (OSTI)

49th International Symposium of Applied Aerodynamics Lille, 24-25-26 March 2014 FP30-2014-toubin on the environment. In order to achieve these ambitious objectives, several ways can be chosen, such as aerodynamic by integrating aerodynamic stresses on the skin (near-field methods), one can equivalently analyze

147

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

E-Print Network (OSTI)

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

McCalley, James D.

148

Aerodynamic Stability and the Growth of Triangular Snow Crystals K. G. Libbrecht and H. M. Arnold  

E-Print Network (OSTI)

Aerodynamic Stability and the Growth of Triangular Snow Crystals K. G. Libbrecht and H. M. Arnold growth perturbations of the more-typical hexagonal forms. We then describe an aerodynamic model leads to air flow around the crystal that promotes the growth of alternating facets. Aerodynamic effects

Libbrecht, Kenneth G.

149

Monitoring the Aerodynamic Efficiency of Intermodal Train Loading Using Machine Vision  

E-Print Network (OSTI)

Monitoring the Aerodynamic Efficiency of Intermodal Train Loading Using Machine Vision TRB 11 transported by North American railroads. Intermodal trains, however, use equipment that is not aerodynamically significant aerodynamic drag. This high resistance associated with the movement of intermodal trains results

Illinois at Urbana-Champaign, University of

150

Aerodynamics of Two Interfering Simple-Shape Bodies in Hypersonic Rarefied-Gas Flows  

E-Print Network (OSTI)

Aerodynamics of Two Interfering Simple-Shape Bodies in Hypersonic Rarefied-Gas Flows Vladimir V and numerical studies [1-4] of aerodynamics of simple shape bodies have provided valuable information related not be used to define the aerodynamics of side-by-side bodies. Flow about two side-by-side cylinders

Riabov, Vladimir V.

151

Aerodynamically Optimal Regional Aircraft Concepts: Conventional and Blended Wing-Body Designs  

E-Print Network (OSTI)

Aerodynamically Optimal Regional Aircraft Concepts: Conventional and Blended Wing-Body Designs aircraft such as those that serve regional routes. We thus explore the optimal aerodynamic shape of both a blended wing-body and conventional tube-and-wing regional aircraft through high-fidelity aerodynamic shape

Zingg, David W.

152

IMPACT OF TIRE AND AERODYNAMIC AIDS ON TRUCK PERFORMANCE ALONG UPGRADE SECTIONS  

E-Print Network (OSTI)

IMPACT OF TIRE AND AERODYNAMIC AIDS ON TRUCK PERFORMANCE ALONG UPGRADE SECTIONS Hesham Rakha1 and aerodynamics aids on the truck acceleration behavior. The objectives of this paper are two-fold. First of vehicle tires, the vehicle's aerodynamic features, the percentage mass on the tractive axle

Rakha, Hesham A.

153

215BAT AERODYNAMICS Revista Chilena de Historia Natural 78: 215-227, 2005  

E-Print Network (OSTI)

215BAT AERODYNAMICS Revista Chilena de Historia Natural 78: 215-227, 2005 Biomechanical and negatively with the mass corrected wingspan and the second component with the aerodynamic efficiency, showing a high aerodynamic efficiency; (3) most of vespertilionids were in the zone of low speed

154

RANS-based Aerodynamic Shape Optimization Investigations of the Common Research Model Wing  

E-Print Network (OSTI)

RANS-based Aerodynamic Shape Optimization Investigations of the Common Research Model Wing Zhoujie of Michigan, Ann Arbor, MI The aerodynamic shape optimization of transonic wings requires Reynolds, and viscous effects. While there has been some research dedicated to RANS-based aerodynamic shape optimiza

Papalambros, Panos

155

SPIE Aerosense, Vol. 4394, paper 108, April 2001 Aerodynamic sampling for landmine trace detection  

E-Print Network (OSTI)

SPIE Aerosense, Vol. 4394, paper 108, April 2001 Aerodynamic sampling for landmine trace detection research on canine olfactory aerodynamics revealed several ways that evolution has dealt with such problems source, 3) use an aerodynamic collar on the sniffer inlet, 4) use auxiliary airjets to stir up surface

Settles, Gary S.

156

Aerodynamic Loads on Tall Buildings: Interactive Database Yin Zhou. M.ASCE1  

E-Print Network (OSTI)

Aerodynamic Loads on Tall Buildings: Interactive Database Yin Zhou. M.ASCE1 ; Tracy Kijewski, S database of aerodynamic loads is presented, which can be accessed by any user with Microsoft Explorer, the nondimensional aerodynamic loads can be used to compute the wind-induced response of tall buildings

Kareem, Ahsan

157

Fluid-Structure Interaction Simulations of a Tension-Cone Inflatable Aerodynamic Decelerator  

E-Print Network (OSTI)

Fluid-Structure Interaction Simulations of a Tension-Cone Inflatable Aerodynamic Decelerator of an aerodynamic tension-cone supersonic decelerator prototype intended for large mass payload deploy- ment. Introduction The concept of the inflatable aerodynamic decelerator (IAD) was first proposed in the 1960's

Cirak, Fehmi

158

The Analysis of Underexpanded Jet Flows for Hypersonic Aerodynamic Experiments in  

E-Print Network (OSTI)

The Analysis of Underexpanded Jet Flows for Hypersonic Aerodynamic Experiments in Vacuum Chambers V of rarefied-gas flows [1]- [3] and aerodynamics of hypersonic probes in wind tunnels [4]-[7]. The objective using quantum concepts [9], [10]. Aerodynamic characteristics of wedges, disks, and plates are studied

Riabov, Vladimir V.

159

Concurrent Aerodynamic Optimization of Rotor Blades Using a Nash Game Method  

E-Print Network (OSTI)

Concurrent Aerodynamic Optimization of Rotor Blades Using a Nash Game Method Enric Roca Le´on Ph Aerodynamics Leader, Airbus Helicopter, Marignane, France Michel Costes Research Engineer, ONERA, Meudon OF THE AMERICAN HELICOPTER SOCIETY Abstract A multi-objective strategy adapted to the aerodynamic concurrent

Paris-Sud XI, Université de

160

PHYSICAL REVIEW E 87, 053021 (2013) Unsteady aerodynamic forces and torques on falling parallelograms in coupled  

E-Print Network (OSTI)

PHYSICAL REVIEW E 87, 053021 (2013) Unsteady aerodynamic forces and torques on falling, these trajectories provide an ideal set of data to analyze 3D aerodynamic force and torque at an intermediate range of Reynolds numbers, and the results will be useful for constructing 3D aerodynamic force and torque models

Wang, Z. Jane

Note: This page contains sample records for the topic "aerodynamic diameter pm" from the National Library of EnergyBeta (NLEBeta).
While these samples are representative of the content of NLEBeta,
they are not comprehensive nor are they the most current set.
We encourage you to perform a real-time search of NLEBeta
to obtain the most current and comprehensive results.


161

Evaluation of the acoustic and aerodynamic constraints of a pneumotachograph for speech and voice studies  

E-Print Network (OSTI)

Evaluation of the acoustic and aerodynamic constraints of a pneumotachograph for speech and voice from its transfer function. 1. INTRODUCTION The measurement of the aerodynamic parameters for the study. The object of this study is to evaluate and correct the acoustic and aerodynamic distortions generated

Paris-Sud XI, Université de

162

GAs for aerodynamic shape design II: multiobjective optimization and multi-criteria design  

E-Print Network (OSTI)

GAs for aerodynamic shape design II: multiobjective optimization and multi-criteria design D, and on their application to multi-criteria design problems. A short introduction to multi- point aerodynamic shape design-lift conditions, and to transonic wing design. 1 Introduction The aerodynamic design problem can be defined

Coello, Carlos A. Coello

163

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

E-Print Network (OSTI)

Error estimation and anisotropic mesh refinement for 3d laminar aerodynamic flow simulations Tobias Leichta,b , Ralf Hartmann,a,b aInstitute of Aerodynamics and Flow Technology, DLR (German Aerospace Center-dimensional laminar aerodynamic flow simulations. The optimal order symmetric interior penalty discontinuous Galerkin

Hartmann, Ralf

164

Development of flexible, intuitive methods for aerodynamic design Type of award PhD Research Studentship  

E-Print Network (OSTI)

Development of flexible, intuitive methods for aerodynamic design Type of award PhD Research is beginning a project to develop new techniques for aerodynamic design. The interest is based around free, they are offering a fully funded 3- year PhD position within the University of Bristol Aerodynamics research group

Bristol, University of

165

Introduction Aerodynamic theory adapted for avian flight (e.g. Tucker,  

E-Print Network (OSTI)

3489 Introduction Aerodynamic theory adapted for avian flight (e.g. Tucker, 1975; Pennycuick, 1989 encompassing optimal foraging and aerodynamic theories. The main hypothesis underlying our model flight strategy selection. We develop a model based on optimal foraging and aerodynamic theories

Loon, E. Emiel van

166

Agricultural and Forest Meteorology 111 (2002) 93108 Estimation of the three-dimensional aerodynamic structure  

E-Print Network (OSTI)

-dimensional aerodynamic structure of a green ash shelterbelt X.H. Zhoua,, J.R. Brandlea, E.S. Takleb,c, C.W. Mized Abstract The three-dimensional aerodynamic structure of a tree shelterbelt is described by two structural be predicted by associating its aerodynamic influence with its struc- ture. The more complex the shelterbelt

Takle, Eugene S.

167

Laboratory Evaluation of Fan-filter Units' Aerodynamic and Energy Performance  

E-Print Network (OSTI)

Laboratory Evaluation of Fan-filter Units' Aerodynamic and Energy Performance Tengfang Xu, Lawrence The paper discusses the benefits of having a consistent testing method to characterize aerodynamic applications. Optimizing aerodynamic performance in air recirculation systems appears to be one of useful

168

Global Optimization Methods for the Aerodynamic Shape Design of Transonic Cascades  

E-Print Network (OSTI)

Global Optimization Methods for the Aerodynamic Shape Design of Transonic Cascades T. Mengistu algorithms, namely Genetic Algorithm (GA) and Simulated Annealing (SA), have been applied to the aerodynamic reduction in total pressure loss by eliminating the passage shock. 1. INTRODUCTION Aerodynamic optimization

Neumaier, Arnold

169

Experimental investigation of the aerodynamic noise radiated by a three-dimensional bluff body  

E-Print Network (OSTI)

Experimental investigation of the aerodynamic noise radiated by a three-dimensional bluff body J.fischer@univ-poitiers.fr Proceedings of the Acoustics 2012 Nantes Conference 23-27 April 2012, Nantes, France 2335 #12;Aerodynamic. The present work is an experimental study of the aerodynamic noise radiated by a three-dimensional simplified

Paris-Sud XI, Université de

170

On the limiting aerodynamic roughness of the ocean in very strong winds  

E-Print Network (OSTI)

On the limiting aerodynamic roughness of the ocean in very strong winds M. A. Donelan,1 B. K. Haus January 2004; accepted 13 August 2004; published 28 September 2004. [1] The aerodynamic friction between, the ``aerodynamic roughness'') increases with the wind speed. Can one merely extrapolate this wind speed tendency

Saltzman, Eric

171

Vocal fold and ventricular fold vibration in period-doubling phonation: Physiological description and aerodynamic  

E-Print Network (OSTI)

and aerodynamic modelinga) Lucie Bailly,b Nathalie Henrich, and Xavier Pelorson Département Parole et Cognition and ventricular areas, the aerodynamic behavior of the laryngeal system is simulated using a simplified physical aerodynamic interaction. Previous experimental in- vestigations dealing with in vitro set

Boyer, Edmond

172

Improvements to a Newton-Krylov Adjoint Algorithm for Aerodynamic Optimization  

E-Print Network (OSTI)

Improvements to a Newton-Krylov Adjoint Algorithm for Aerodynamic Optimization David W. Zingg-based algorithm for aerodynamic optimization. A Newton-Krylov algorithm is used to solve the compressible Navier of the improvements on the performance of the algorithm is presented. I. Introduction Numerical aerodynamic shape

Zingg, David W.

173

Surface-Skimming Stoneflies and Mayflies: The Taxonomic and Mechanical Diversity of Two-Dimensional Aerodynamic  

E-Print Network (OSTI)

-Dimensional Aerodynamic Locomotion* James H. Marden Brigid C. O'Donnell Michael A. Thomas Jesse Y. Bye Department be used to accomplish two-dimensional aerodynamic locomotion on the surface of water. Here we extend, horizontal velocity, and the verticality of aerodynamic force production increase as the body orientation

Marden, James

174

Aerodynamic focusing of high-density aerosols D.E. Ruiz a,n  

E-Print Network (OSTI)

Aerodynamic focusing of high-density aerosols D.E. Ruiz a,n , L.M. Gunderson a , M.J. Hay a , E Accepted 24 May 2014 Available online 17 June 2014 Keywords: Aerodynamic lens High-density aerosol beam recover previous findings on aerodynamic focusing at low densities. At higher densities

175

Advances in Modeling of Aerodynamic Forces on Bridge Xinzhong Chen1  

E-Print Network (OSTI)

Advances in Modeling of Aerodynamic Forces on Bridge Decks Xinzhong Chen1 and Ahsan Kareem2 Abstract: Aerodynamic forces on bridges are commonly separated into static, self-excited, and buffeting in modeling aerodynamic forces. Formulations for airfoil sections and those based on quasi- steady theory

Chen, Xinzhong

176

Development of New Grid-Fin Design for Aerodynamic Marco Debiasi1  

E-Print Network (OSTI)

1 Development of New Grid-Fin Design for Aerodynamic Control Marco Debiasi1 Temasek Laboratories of attack = angle of the sharp leading edge = swept-back angle I. Introduction grid fin is an aerodynamic Aerodynamics Conference, Chicago, Illinois, 28 June - 1 July 2010, and as Paper 2012-2909 at the 30th AIAA

Debiasi, Marco

177

Determination of the Aerodynamic Characteristics of Low Reynolds Number Flows over Small Uninhabited Aerial Vehicles  

E-Print Network (OSTI)

Determination of the Aerodynamic Characteristics of Low Reynolds Number Flows over Small, in the 15000 - 500000 range. The high Re aerodynamics is well established, however the same cannot be said for the low Re regime. In this range the wing's aerodynamic performance can deteriorate rapidly as the Re

Olsen, Stephen L.

178

Design Optimization of MultiElement Aerodynamic Configurations Using a Viscous  

E-Print Network (OSTI)

Design Optimization of Multi­Element Aerodynamic Configurations Using a Viscous Adjoint Method.S.A An adjoint-based Navier-Stokes design and optimization method for multi-element aerodynamic configurations effects. Using a viscous continuous adjoint formulation, the necessary aerodynamic gradient information

Kim, Sangho

179

Aerodynamic and aeroacoustic analysis of morphing Type of award PhD Research Studentship  

E-Print Network (OSTI)

Aerodynamic and aeroacoustic analysis of morphing structures Type of award PhD Research Studentship with a strong interest in aerodynamics. Deadline Open until filled. PhD Topic Background/Description Applications are invited for a research studentship in the field of aerodynamics and aeroacoustics, leading

Bristol, University of

180

NONLINEAR AERODYNAMIC ANALYSIS OF BRIDGES UNDER TURBULENT WINDS: THE NEW FRONTIER IN BRIDGE  

E-Print Network (OSTI)

NONLINEAR AERODYNAMIC ANALYSIS OF BRIDGES UNDER TURBULENT WINDS: THE NEW FRONTIER IN BRIDGE AERODYNAMICS Xinzhong Chen , Ahsan Kareem and Fred L. Haan, Jr. ¡ Department of Civil Engineering. These approaches are limited to linear structures in which nonlinearities in aerodynamic forces are ignored

Kareem, Ahsan

Note: This page contains sample records for the topic "aerodynamic diameter pm" from the National Library of EnergyBeta (NLEBeta).
While these samples are representative of the content of NLEBeta,
they are not comprehensive nor are they the most current set.
We encourage you to perform a real-time search of NLEBeta
to obtain the most current and comprehensive results.


181

Current trends in modelling research for turbulent aerodynamic flows  

Science Journals Connector (OSTI)

...specific heats (c p/c v) and R is the gas constant. The presence of the turbulent...over and downstream of airfoils, wings, turbine blades or aerodynamic bodies. It is necessary...Navier-Stokes equations: properties of the residual stress. Phys. Fluids. 15, 2127-2140...

2007-01-01T23:59:59.000Z

182

Aerodynamic Drag Reduction Apparatus For Wheeled Vehicles In Ground Effect  

DOE Patents (OSTI)

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.

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

2005-12-13T23:59:59.000Z

183

Aerodynamic performance measurements of a film-cooled turbine stage  

E-Print Network (OSTI)

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 ...

Keogh, Rory (Rory Colm), 1968-

2001-01-01T23:59:59.000Z

184

Aerodynamic Optimization Under a Range of Operating Conditions  

E-Print Network (OSTI)

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

Zingg, David W.

185

Adapting to Limitations of a Wind Tunnel Test Facility in the Aerodynamic Testing of a new UAV  

E-Print Network (OSTI)

Adapting to Limitations of a Wind Tunnel Test Facility in the Aerodynamic Testing of a new UAV Dr K section for aerodynamic tests of aircraft models and aerodynamic devices. Improvements over the years have aerodynamic testing facility, albeit with much reduced capability. This paper reports on initial progress

Wong, K. C.

186

THE SYNTENIC DIAMETER OF THE SPACE OF NCHROMOSOME  

E-Print Network (OSTI)

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

Kleinberg, Jon

187

Linear PM Generator for Wave Energy Conversion.  

E-Print Network (OSTI)

??The main objective of this thesis is to design a selected version of linear PM generator and to determine the electromechanical characteristics at variable operating… (more)

Parthasarathy, Rajkumar

2012-01-01T23:59:59.000Z

188

SWIMMING POOL Monday-Thursday: 12-8pm  

E-Print Network (OSTI)

SWIMMING POOL Monday-Thursday: 12-8pm Friday: 12-5pm GYM 121 FALL 2012 OCTOBER 15th-DECEMBER 14th *NEW* Hip Hop 12-1pm (GYM 100C) -Susan Turbo Kick® 12-1pm (GYM 100J) -Laura Aqua Fit 12-1pm (Pool) -AQ (Pool) -AQ Staff H2O Aerobics 6-7pm (Pool) -AQ Staff Hatha Yoga Flow 12-1pm (BH6) -Meredith ZUMBA® 12

189

Predicting aerodynamic characteristic of typical wind turbine airfoils using CFD  

SciTech Connect

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.

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

1997-09-01T23:59:59.000Z

190

Performance evaluation of PM?? and high-volume air samplers using a Coulter Counter Particle Size Analyzer  

E-Print Network (OSTI)

by the HiVol/Coulter process. The HiVol/Coulter process includes the determination of the percent of particles less than 10 um (AED) on a total suspended particulate matter filter. Representative particle size distributions were obtained for cotton dust... with an aerodynamic equivalent diameter (AED) larger than 10 micrometers (um) were seldom found in the air spaces of the lungs, Particles larger than 10 um (AED) do not pass the filtering mechanisms of the respiratory tract and are of less concern (AMA, 1963...

Herber, Douglas John

2012-06-07T23:59:59.000Z

191

Complete genomic sequence of Pasteurella multocida,Pm70  

Science Journals Connector (OSTI)

...chain A dmsA PM1755 anaerobic dimethyl sulfoxide reductase, chain B dmsB PM1756 anaerobic dimethyl sulfoxide reductase, chain C dmsC ATP-proton motive force interconversion PM1488 ATP synthase, a chain atpB PM1489 ATP synthase, c chain atpE PM1490 ATP synthase...

Barbara J. May; Qing Zhang; Ling Ling Li; Michael L. Paustian; Thomas S. Whittam; Vivek Kapur

2001-01-01T23:59:59.000Z

192

E-Print Network 3.0 - aerodynamic noise propagation Sample Search...  

NLE Websites -- All DOE Office Websites (Extended Search)

Collection: Biology and Medicine 5 AIAA-2004-1184 AN AEROACOUSTIC ANALYSIS OF WIND TURBINES* Summary: noise, the aerodynamics and aeroacoustics of rotating blades, and the...

193

E-Print Network 3.0 - aero-elasticity rotor aerodynamics Sample...  

NLE Websites -- All DOE Office Websites (Extended Search)

Summary: HVDC 12;Rotor aero-elastics and structural dynamics 12;Aerodynamics for wind turbines Flow over... and components Rotor aero-elastics and structural dynamics Grid...

194

DOEs Effort to Reduce Truck Aerodynamic Drag through Joint...  

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

Experiments DOEs Effort to Reduce Truck Aerodynamic Drag through Joint Experiments Presentation from the U.S. DOE Office of Vehicle Technologies "Mega" Merit Review 2008 on...

195

E-Print Network 3.0 - aerodynamic design optimization Sample...  

NLE Websites -- All DOE Office Websites (Extended Search)

Search Powered by Explorit Topic List Advanced Search Sample search results for: aerodynamic design optimization Page: << < 1 2 3 4 5 > >> 1 Aerospace Engineering Online by the...

196

DOEs Effort to Reduce Truck Aerodynamic Drag through Joint...  

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

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

197

DOEs Effort to Reduce Truck Aerodynamic Drag through Joint...  

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

Experiments and Computations DOEs Effort to Reduce Truck Aerodynamic Drag through Joint Experiments and Computations 2010 DOE Vehicle Technologies and Hydrogen Programs Annual...

198

E-Print Network 3.0 - aerodynamics performance cooling Sample...  

NLE Websites -- All DOE Office Websites (Extended Search)

Airfoil Summary: Design Ahmed Abdelwahab Manager of Turbomachinery Aerodynamics Praxair Inc., Global Supply System... are compared. The analysis is presented both in terms...

199

E-Print Network 3.0 - aerodynamics final technical Sample Search...  

NLE Websites -- All DOE Office Websites (Extended Search)

Airfoil Summary: Design Ahmed Abdelwahab Manager of Turbomachinery Aerodynamics Praxair Inc., Global Supply System... as the detailed flow-field features. Finally Concluding...

200

E-Print Network 3.0 - aerodynamic noise reduction Sample Search...  

NLE Websites -- All DOE Office Websites (Extended Search)

Control Seminar Series The Dynamics, Systems, and Control Seminar covers a broad range of topics of interest to the Summary: aerodynamic efficiency due to the reduction of induce...

Note: This page contains sample records for the topic "aerodynamic diameter pm" from the National Library of EnergyBeta (NLEBeta).
While these samples are representative of the content of NLEBeta,
they are not comprehensive nor are they the most current set.
We encourage you to perform a real-time search of NLEBeta
to obtain the most current and comprehensive results.


201

E-Print Network 3.0 - aerodynamic size separator Sample Search...  

NLE Websites -- All DOE Office Websites (Extended Search)

Control Seminar Series The Dynamics, Systems, and Control Seminar covers a broad range of topics of interest to the Summary: proximity aerodynamics information between two UAVs at...

202

PM PEM’s Pre-Measurement Allowance – On-Road Evaluation and Investigation  

E-Print Network (OSTI)

FID PM balance PM filter temperature CVS propane check PMfilter sample flow propane check PM sample flow meter PMPM filter temperature CVS propane check PM filter sample

Durbin, T; Jung, H; Cocker III, D R; Johnson, K

2009-01-01T23:59:59.000Z

203

PM PEM’s On-Road Investigation – With and Without DPF Equipped Engines  

E-Print Network (OSTI)

with 6 connections). pass Propane CVS verification pass,FID PM balance PM filter temperature CVS propane check PMfilter sample flow propane check PM sample flow meter PM

Durbin, T; Jung, H; Cocker III, D R; Johnson, K

2009-01-01T23:59:59.000Z

204

Low Cost PM Technology for Particle Reinforced Titanium Automotive...  

Energy.gov (U.S. Department of Energy (DOE)) Indexed Site

Low Cost PM Technology for Particle Reinforced Titanium Automotive Components: Manufacturing Process Feasibility StudyAMD 310 Low Cost PM Technology for Particle Reinforced...

205

An Improvement of Diesel PM and NOx Reduction System | Department...  

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

& Publications Development on simultaneous reduction system of NOx and PM from a diesel engine An Improvement of Diesel PM and NOx Reduction System New Diesel Emissions...

206

Development on simultaneous reduction system of NOx and PM from...  

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

More Documents & Publications An Improvement of Diesel PM and NOx Reduction System An Improvement of Diesel PM and NOx Reduction System EPA Mobile Source Rule Update...

207

Validation Testing for the PM-PEMS Measurement Allowance Program  

E-Print Network (OSTI)

13 Table 2-10 UCR primary and secondary propane recoveryand secondary dilution tunnel propane recover tests werePM filter temperature CVS propane check PM filter sample

Johnson, K; Durbin, T; Jung, H; Cocker III, D R; Khan, M Y

2010-01-01T23:59:59.000Z

208

Virtual Oxygen Sensor for Innovative NOx and PM Emission Control...  

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

Virtual Oxygen Sensor for Innovative NOx and PM Emission Control Technologies Virtual Oxygen Sensor for Innovative NOx and PM Emission Control Technologies A virtual O2 sensor for...

209

James Webb Space Telescope: PM Lessons Applied - Eric Smith,...  

Energy Savers (EERE)

James Webb Space Telescope: PM Lessons Applied - Eric Smith, Deputy Program Director, NASA James Webb Space Telescope: PM Lessons Applied - Eric Smith, Deputy Program Director,...

210

DOE's Gasoline/Diesel PM Split Study | Department of Energy  

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

GasolineDiesel PM Split Study DOE's GasolineDiesel PM Split Study 2005 Diesel Engine Emissions Reduction (DEER) Conference Presentations and Posters 2005deerfujita.pdf More...

211

Aerodynamic design considerations for a free-flying ducted propeller  

SciTech Connect

The design philosophy for a free-flying vehicle powered by a ducted propeller is presented from an aerodynamic viewpoint. Airframe design concentrates on duct inlet lip curvature, diffuser angle, and methods of vehicle control. Wind tunnel test results are given to evaluate two inlet designs, two exit designs, and the effect of external appendages such as a camera pod or a forebody. Finally, a simple, analytic method of ducted propeller blade design is presented and the results compared with an existing ducted propeller blade. 14 refs., 28 figs., 2 tabs.

Weir, R.J.

1988-01-01T23:59:59.000Z

212

The 5-megawatt power plant with 126 metre rotor diameter  

E-Print Network (OSTI)

The 5-megawatt power plant with 126 metre rotor diameter #12;Design data Rated power 5,000kW Cut-in speed 3.5m/s Rated wind speed 13.0m/s Cut-out speed 25.0m/s onshore 30.0m/s offshore Wind zone up to DIBt 3 Type class up to IEC Ib / GL offshore type class I Rotor Diameter 126.0m Rotor area 12,469m2

Firestone, Jeremy

213

Journal of Industrial Aerodynamics, 3 (1978) 251--257 251 Elsevier Scientific Publishing Company, Amsterdam --Printed in The Netherlands  

E-Print Network (OSTI)

Journal of Industrial Aerodynamics, 3 (1978) 251--257 251 © Elsevier Scientific Publishing Company strong vortices. Both of these properties were used in the design of the aerodynamic dampers which

Hunt, Julian

214

Bericht des Instituts f ur Aerodynamik und Str omungstechnik Report of the Institute of Aerodynamics and Flow Technology  

E-Print Network (OSTI)

of Aerodynamics and Flow Technology IB 124-2008/1 Discontinuous Galerkin Methods for inviscid low Mach number of Alessandra Nigro at the Institute of Aerodynamics and Flow Technology at the DLR, Braunschweig. This work has

Hartmann, Ralf

215

A Computational Method for Determining Distributed Aerodynamic Loads on Planforms of Arbitrary Shape in Compressible Subsonic Flow  

E-Print Network (OSTI)

The methods presented in this work are intended to provided an easy to understand and easy to apply method for determining the distributed aerodynamic loads and aerodynamic characteristics of planforms of nearly arbitrary shape. Through application...

Brown, Matthew Alan

2013-12-31T23:59:59.000Z

216

Tracking an Aerodynamic Model in a Wind Tunnel with a Stereo High-speed Imaging System  

E-Print Network (OSTI)

Tracking an Aerodynamic Model in a Wind Tunnel with a Stereo High-speed Imaging System Lichuan Gui in wind tunnel tests with a stereo high-speed imaging system. The imaging system includes two high angle, pitch angle and yaw angle of the aerodynamic model in the wind tunnel. Tests and simulations were

Gui, Lichuan

217

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

E-Print Network (OSTI)

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. On the other hand, the characteristics of unsteady flow around the helical wind turbine were studied with a hot

Leu, Tzong-Shyng "Jeremy"

218

Viscosity, hard sphere diameter and interionic potential for liquid lead  

E-Print Network (OSTI)

L-347 Viscosity, hard sphere diameter and interionic potential for liquid lead G. Chaussemy The Macedo-Litovitz equation for a hard sphere liquid provides a satisfactory model for the viscosity of lead and molecular dynamics. The activation energy for viscosity (0.07 eV) is similar to the height of the interionic

Boyer, Edmond

219

Offshore Series Wind Turbine Variable Hub heights & rotor diameters  

E-Print Network (OSTI)

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

Firestone, Jeremy

220

Advanced numerical methods for analysis and design in aircraft aerodynamics  

Science Journals Connector (OSTI)

A review is presented of developments in recent years in computational methods for aerodynamic design and analysis. The discussion is mainly influenced by the industrial requirements and developments at Dornier. The need and use of computational aerodynamics in the design of aircraft and missile configurations is explored through several examples. These include synthesis-programs and predesign and evaluation work of aircraft and missile weapon systems, airfoil and high lift analysis and deign methodologies, three-dimensional transport- and fighter aircraft wing-body analysis methods for the complete speed range from subsonic to supersonic speed even including leading edge vortex flows, engine-inlet flows and interference problems. Besides the importance of advanced numerical schemes and fast large computers the cost-limiting factor of complex geometry handling and data pre- and post-processing is discussed. The use of these numerical methods has proved to substantially increase aircraft performance capabilities while reducing risk, flow time, and testing requirements and thus total costs. At the same time such methods are in use to analyse and improve current and future wind tunnel limitations like wall effects, flow angularity, and Reynolds number.

W. Schmidt

1986-01-01T23:59:59.000Z

Note: This page contains sample records for the topic "aerodynamic diameter pm" from the National Library of EnergyBeta (NLEBeta).
While these samples are representative of the content of NLEBeta,
they are not comprehensive nor are they the most current set.
We encourage you to perform a real-time search of NLEBeta
to obtain the most current and comprehensive results.


221

Wind turbine trailing-edge aerodynamic brake design  

SciTech Connect

This report describes the design of a centrifugally actuated aerodynamic-overspeed device for a horizontal-axis wind turbine. The device will meet the following criteria; (1) It will be effective for airfoil angles of attack 0{degrees} to 45{degrees}. (2) It will be stowed inside the blade profile prior to deployment. (3) It will be capable of offsetting the positive torque produced by the overall blade. (4) Hinge moments will be minimized to lower actuator loads and cost. (5) It will be evaluated as a potential power modulating active rotor-control system. A literature review of aerodynamic braking devices was conducted. Information from the literature review was used to conceptualize the most effective devices for subsequent testing and design. Wind-tunnel test data for several braking devices are presented in this report. Using the data for the most promising configuration, a preliminary design was developed for a MICON 65/13 wind turbine with Phoenix 7.9-m rotor blades.

Quandt, G.

1996-01-01T23:59:59.000Z

222

American Institute of Aeronautics and Astronautics Paper 2009-1299 Unsteady Aerodynamics and Wing Kinematics Effect in  

E-Print Network (OSTI)

1 American Institute of Aeronautics and Astronautics Paper 2009-1299 Unsteady Aerodynamics and Wing of unsteady aerodynamic mechanisms such as wake capture, leading-edge vortex, Weis­Fogh "clap aerodynamics are of particular interests in this study. Simulations have shown that the vortex topologies

223

Estimation of the aerodynamic roughness length in arid and semi-arid regions over the globe with the ERS scatterometer  

E-Print Network (OSTI)

Estimation of the aerodynamic roughness length in arid and semi-arid regions over the globe 2005. [1] Estimates of the aerodynamic roughness lengths z0 in arid and semi-arid regions: Prigent, C., I. Tegen, F. Aires, B. Marticorena, and M. Zribi (2005), Estimation of the aerodynamic

Aires, Filipe

224

An empirical expression to relate aerodynamic and surface temperatures for use within1 single-source energy balance models2  

E-Print Network (OSTI)

1 n.1 An empirical expression to relate aerodynamic and surface temperatures for use within1 single that the14 reference temperature for the estimation of convective fluxes, the aerodynamic temperature, is15 between the aerodynamic22 and the air temperatures and the difference between the surface and the air

Paris-Sud XI, Université de

225

STAGGEREDMESH COMPUTATION FOR AERODYNAMIC G.S. Djambazov \\Lambda , C.H. Lai y & K.A. Pericleous z  

E-Print Network (OSTI)

STAGGERED­MESH COMPUTATION FOR AERODYNAMIC SOUND G.S. Djambazov \\Lambda , C.­H. Lai y & K the applicability of a combined technique for aerodynamic sound simulation based on the staggered acoustic routines in magnitude and scale of the quantities involved. Aerodynamic sound is generated as a result

Lai, Choi-Hong

226

Marques, Flvio Donizeti (1997) Multi-layer functional approximation of non-linear unsteady aerodynamic response. PhD thesis.  

E-Print Network (OSTI)

aerodynamic response. PhD thesis. http://theses.gla.ac.uk/2091/ Copyright and moral rights for this thesis-LAYER FUNCTIONAL APPROXIMATION OF NON-LINEAR UNSTEADY AERODYNAMIC RESPONSE by Flavio Donizeti Marques Thesis 1997 CopYright 1997 Flavio Donizet i Marques, #12;Abstract Non-linear unsteady aerodynamic effects

Glasgow, University of

227

Complete genomic sequence of Pasteurella multocida,Pm70  

Science Journals Connector (OSTI)

...of Pm, Hi, and Ec for the 1,197 orthologs. The mean (±standard deviation) of the pairwise distances were: Pm-Hi 56.6 ± 83...dmsB PM1756 anaerobic dimethyl sulfoxide reductase, chain C dmsC ATP-proton motive force interconversion PM1488 ATP synthase...

Barbara J. May; Qing Zhang; Ling Ling Li; Michael L. Paustian; Thomas S. Whittam; Vivek Kapur

2001-01-01T23:59:59.000Z

228

Drilling Large Diameter Holes in Rocks Using Multiple Laser Beams  

NLE Websites -- All DOE Office Websites (Extended Search)

Drilling Large Diameter Holes in Rocks Using Multiple Laser Beams (504) Drilling Large Diameter Holes in Rocks Using Multiple Laser Beams (504) Richard Parker,. Parker Geoscience Consulting, LLC, Arvada, Colorado, USA; Zhiyue Xu and Claude Reed, Argonne National Laboratory, Argonne, Illinois, USA; Ramona Graves, Department of Petroleum Engineering, Colorado School of Mines, Golden, Colorado, USA; Brian Gahan and Samih Batarseh, Gas Technology Institute, Des Plaines, Illinois, USA ABSTRACT Studies on drilling petroleum reservoir rocks with lasers show that modern infrared lasers have the capability to spall (thermally fragment), melt and vaporize natural earth materials with the thermal spallation being the most efficient rock removal mechanism. Although laser irradiance as low as 1000 W/cm 2 is sufficient to spall rock, firing the

229

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)

Cavitation as a complementary tool for automotive aerodynamics J.F. Beaudoin, O. Cadot, J.L. Aider consists in reducing the aerodynamic drag of the vehicles. As a matter of fact, aerodynamic forces play and Sovran 1993; Hucho 1998). Since the pioneering work of Morel (1978) and Ahmed (1983) about aerodynamics

Wesfreid, José Eduardo

230

Finding the Force -- Consistent Particle Seeding for Satellite Aerodynamics  

E-Print Network (OSTI)

When calculating satellite trajectories in low-earth orbit, engineers need to adequately estimate aerodynamic forces. But to this day, obtaining the drag acting on the complicated shapes of modern spacecraft suffers from many sources of error. While part of the problem is the uncertain density in the upper atmosphere, this works focuses on improving the modeling of interacting rarified gases and satellite surfaces. The only numerical approach that currently captures effects in this flow regime---like self-shadowing and multiple molecular reflections---is known as test-particle Monte Carlo. This method executes a ray-tracing algorithm to follow particles that pass through a control volume containing the spacecraft and accumulates the momentum transfer to the body surfaces. Statistical fluctuations inherent in the approach demand particle numbers in the order of millions, often making this scheme too costly to be practical. This work presents a parallel test-particle Monte Carlo method that takes advantage of b...

Parham, J Brent

2013-01-01T23:59:59.000Z

231

Vacuum chamber with a supersonic-flow aerodynamic window  

DOE Patents (OSTI)

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.

Hanson, C.L.

1980-10-14T23:59:59.000Z

232

Vacuum chamber with a supersonic flow aerodynamic window  

DOE Patents (OSTI)

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.

Hanson, Clark L. (Livermore, CA)

1982-01-01T23:59:59.000Z

233

Force control system design for aerodynamic load simulator  

Science Journals Connector (OSTI)

A dynamic load simulator which can reproduce on-ground the aerodynamic hinge moment of control surface is an essential rig for the performance and stability test of an aircraft actuation system. The hinge moment varies widely over the flight envelope depending on the specific flight condition and maneuvering status. To replicate the wide spectrum of this hinge moment variation within some accuracy bounds, a force controller is designed based on the quantitative feedback theory (QFT). A dynamic model of load actuation system is derived, and verified through the experiment. The efficacy of QFT force controller is verified by a numerical simulation, in which combined aircraft dynamics, flight control law and hydraulic actuation system dynamics of aircraft control surface are considered.

Yoonsu Nam; Sung Kyung Hong

2002-01-01T23:59:59.000Z

234

Joint computational and experimental aerodynamics research on a reentry vehicle  

SciTech Connect

This paper seeks to improve the synergism between computational aerodynamics and wind tunnel experimentation. In this paper, experimental and computational results are presented for a hypersonic vehicle configuration at Mach 8. Comparisons are made between experimental and computational results in order to improve the accuracy of both approaches. The basic vehicle configuration is a spherically blunted cone with a slice parallel with the axis of the vehicle. The half-angle of the cone is 10 deg. and the ratio of spherical nose radius to base radius in 10%. Onto the slice portion of the vehicle can be attached flaps with three different deflection angles; 10, 20, and 30 deg. All of the experimental results were obtained in the Sandia Mach 8 long duration, blow-down, hypersonic wind tunnel. Flow visualization results include surface oil flow, spark schlieren, and liquid crystal photographs and video. The liquid crystals were used as an aid in verifying that a laminar boundary layer existed over the entire body. An extensive uncertainty analysis was conducted to estimate quantitatively the accuracy of the measurement. Computational aerodynamic force and moment predictions are compared with the wind tunnel data. The Sandia Parabolized Navier-Stokes code is used to generate solutions for the sliced vehicle (no flap) and partial solutions for the flapped vehicle. For the geometry with the flap, an axially separated flow occurs and a time iterative Navier-Stokes code is used to provide comparisons with the data. This paper presents a portion of the results given in earlier works and also discusses new experimental results with this configuration.

Not Available

1991-01-01T23:59:59.000Z

235

Aerodynamic effects in ink-jet printing on a moving web  

E-Print Network (OSTI)

Hsiao, W.-K., Hoath, S.D., Martin, G.D. and Hutchings, I.M., paper for NIP28 2012, 'Aerodynamic effects in ink-jet printing on a moving web' (accepted) Aerodynamic Effects in Ink-Jet Printing on a Moving Web Wen-Kai Hsiao, Stephen D Hoath... airflow and the wakes from the printed ink drops should be investigated as the primary source of aerodynamically-related print quality issues. Introduction The scope of commercial ink-jet printing has extended significant- ly in recent years. For new...

Hsiao, W.-K.; Hoath, S.D.; Martin, G.D.; Hutchings, I.M.

2012-01-01T23:59:59.000Z

236

Aerodynamic performance and characteristic of vortex structures for Darrieus wind turbine. II. The relationship between vortex structure and aerodynamic performance  

Science Journals Connector (OSTI)

In this paper transient computational fluid dynamics (CFD) simulations of a straight-bladed Darrieus type vertical axis wind turbine were performed by means of an in-house CFD code. The Spalart-Allmaras turbulence model was implemented in the numerical code for the turbulence. Particular emphasis was placed on effect of interaction between vortices and blades on the aerodynamic performance of the simulated turbine at different tip speed and solidity ratios. The obtained results suggested that vortices were shed from previous blade passages and the close encounter of a rotor blade with these vortices can have a considerable impact on power coefficient of the simulated turbine during operation at different tip speed ratios. As a result possible reasons for the changes in the behavior of this type of turbine due to the variation of tip speed ratio and solidity were proposed.

2014-01-01T23:59:59.000Z

237

A Case Study of Wide Diameter Casing for Geothermal Systems  

SciTech Connect

Three wells have been drilled in the central resistivity area of a geothermal field in the Taupo Volcanic Zone, New Zealand. Using a well bore simulator, WELL SIM V3.0, reservoir conditions and well characteristics are evaluated to determine the increase in output by increasing production casing diameters from either 8-5/8 inches OD or 9-5/8 inches OD to 13-3/8 inches OD. Increases in well drilling costs are determined to provide a commentary on the economics. While open hole size is effectively doubled, well costs increase by 10% and, in this study, output increases by an average of 18%.

King, T.R.; Freeston, D.H.; Winmill, R.L.

1995-01-01T23:59:59.000Z

238

Ted Sargent PhD Thursday, JAN. 17, 2013 3PM to 4PM  

E-Print Network (OSTI)

Hall Refreshments Before Seminar at 2:45PM Optoelectronic Devices Based on Colloidal Quantum Dot Solids to colloidal quantum dot optoelectronic devices." He is a KAUST Investigator; and is CTO of In

239

Aerodynamic Losses and Heat Transfer in a Blade Cascade with 3-D Endwall Contouring  

NLE Websites -- All DOE Office Websites (Extended Search)

Aerodynamic Losses and Heat Transfer in a Aerodynamic Losses and Heat Transfer in a Aerodynamic Losses and Heat Transfer in a Aerodynamic Losses and Heat Transfer in a Blade Cascade with 3 Blade Cascade with 3 - - D D Endwall Endwall Contouring Contouring Principal Investigator Principal Investigator Sumanta Acharya, Professor Sumanta Acharya, Professor Louisiana State University, Baton Rouge, Louisiana Louisiana State University, Baton Rouge, Louisiana Collaborators Collaborators Gazi Mahmood, Ph.D., Research Asqociate Gazi Mahmood, Ph.D., Research Asqociate Arun Saha, Ph.D., Research Associate Arun Saha, Ph.D., Research Associate Ross Gustafson, M.S. student Ross Gustafson, M.S. student SCIES Project 02 SCIES Project 02 - - 01 01 - - SR098 SR098 DOE COOPERATIVE AGREEMENT DE DOE COOPERATIVE AGREEMENT DE - - FC26 FC26 - - 02NT41431 02NT41431 Tom J. George, Program Manager, DOE/NETL

240

Influence of low-speed aerodynamic performance on airport community noise  

E-Print Network (OSTI)

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 ...

March, Andrew I. (Andrew Irving)

2008-01-01T23:59:59.000Z

Note: This page contains sample records for the topic "aerodynamic diameter pm" from the National Library of EnergyBeta (NLEBeta).
While these samples are representative of the content of NLEBeta,
they are not comprehensive nor are they the most current set.
We encourage you to perform a real-time search of NLEBeta
to obtain the most current and comprehensive results.


241

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

E-Print Network (OSTI)

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...

Lykins, Ryan

2014-05-31T23:59:59.000Z

242

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

E-Print Network (OSTI)

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...

Lee, Hyunjung

2010-03-29T23:59:59.000Z

243

E-Print Network 3.0 - aerodynamic shape design Sample Search...  

NLE Websites -- All DOE Office Websites (Extended Search)

Search Powered by Explorit Topic List Advanced Search Sample search results for: aerodynamic shape design Page: << < 1 2 3 4 5 > >> 1 For more information or to apply, contact...

244

Aerodynamics of Two Interfering Simple-Shape Bodies in Hypersonic Rarefied-Gas Flows  

E-Print Network (OSTI)

Aerodynamics of Two Interfering Simple-Shape Bodies in Hypersonic Rarefied-Gas Flows Vladimir V. Riabov Rivier College, Nashua, New Hampshire, USA ABSTRACT Hypersonic rarefied-gas flows near two side of Hypersonic Rarefied Gas Flows n

Riabov, Vladimir V.

245

E-Print Network 3.0 - aerodynamic heating computations Sample...  

NLE Websites -- All DOE Office Websites (Extended Search)

Control Seminar Series The Dynamics, Systems, and Control Seminar covers a broad range of topics of interest to the Summary: will be served. May 6th, 2010 Edgar Cuji "Aerodynamic...

246

How to improve open rotor aerodynamics at cruise and take-off  

E-Print Network (OSTI)

1 Copyright © 2014 University of Cambridge DRAFT – HOW TO IMPROVE OPEN ROTOR AERODYNAMICS AT CRUISE AND TAKE-OFF Cesare Hall, Alexios Zachariadis, Tobias Brandvik, Nishad Sohoni cah1003@cam.ac.uk University of Cambridge, Whittle... Laboratory 1 JJ Thomson Avenue, Cambridge CB3 0DY ABSTRACT A key challenge in open rotor design is getting the optimum aerodynamics at both the cruise and take-off conditions. This is particularly difficult because the operation and the requirements...

Hall, Cesare; Zachariadis, Alexios; Brandvik, Tobias; Sohoni, Nishad

247

Effect of aerodynamic uncertainties on unconventional lateral control at high angle of attack  

E-Print Network (OSTI)

EFFECT OF AERODYNAMIC UNCERTAINTIES ON UNCONVENTIONAL LATERAL CONTROL AT HIGH ANGLE OF ATTACK A Thesis by BOB GENSEN ELLER Submitted to the Graduate College of Texas ARM University in partial fulfillment of the requirement for the degree... of MASTER OF SCIENCE December 1987 Major Subject: Aerospace Engineering EFFECT OF AERODYNAMIC UNCERTAINTIES ON UNCONVENTIONAL LATEHAI CONTROL AT HIGH ANGI. E (&F A'I'TACK A Thesis by BOB GENSEN ELLER Approved as to style and content by: Donald T...

Eller, Bob Gensen

1987-01-01T23:59:59.000Z

248

An aerodynamic surface to deploy and position a stall deterrent spoiler  

E-Print Network (OSTI)

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...

Brown, Jeffrey Reed

1974-01-01T23:59:59.000Z

249

Computer subroutine for estimating aerodynamic blade loads on Darrieus vertical axis wind turbines. [FORCE code  

SciTech Connect

An important aspect of structural design of the Darrieus rotor is the determination of aerodynamic blade loads. This report describes a load generator which has been used at Sandia for quasi-static and dynamic rotor analyses. The generator is based on the single streamtube aerodynamic flow model and is constructed as a FORTRAN IV subroutine to facilitate its use in finite element structural models. Input and output characteristics of the subroutine are described and a complete listing is attached as an appendix.

Sullivan, W. N.; Leonard, T. M.

1980-11-01T23:59:59.000Z

250

An Experimental Study of PM Emission Characteristics of Commercial...  

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

Study of PM Emission Characteristics of Commercial Diesel Engine with Urea-SCR System An Experimental Study of PM Emission Characteristics of Commercial Diesel Engine with Urea-SCR...

251

DOE's Gasoline/Diesel PM Split Study | Department of Energy  

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

Desert Research Institute 2003deerfujita.pdf More Documents & Publications DOE's GasolineDiesel PM Split Study DOE's GasolineDiesel PM Split Study Long-Term Changes in Gas-...

252

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

E-Print Network (OSTI)

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...

McClure, Joshua Wayne

2012-06-07T23:59:59.000Z

253

Large Eddy Simulation of wind farm aerodynamics: A review  

Science Journals Connector (OSTI)

Abstract To study wind farm aerodynamics (WFA), the Wind Power industry currently relies on simple Engineering Models (EM) that simulate wind farms using basic principles of physics and empirically established approximations. \\{EMs\\} are fast and accurate for an overview of WFA and gauging mean power production, but cannot resolve phenomena like wake meandering, effect of atmospheric stratification on wake development, a turbine?s response to partial wake interaction and yawed inflows etc., and their relation with turbine loading, which require a first principle physics-based model, namely Computational Fluid Dynamics (CFD). Although advances in computer technology have promoted the application of CFD, the study of WFA is yet unworkable with Direct Numerical Simulation, which is the most comprehensive CFD technique. Thus, as a trade-off between cost and detail, researchers must resort to Large Eddy Simulation (LES) to garner thorough knowledge of WFA, which could in succession help the industry improve engineering models. This paper summarises the contributions of various LES investigations into WFA and how they have helped broaden our understanding of the subject. Additionally, the article touches upon the optimal use of LES and of the resultant data, and also the challenges faced by LES.

D. Mehta; A.H. van Zuijlen; B. Koren; J.G. Holierhoek; H. Bijl

2014-01-01T23:59:59.000Z

254

Tandem Differential Mobility Analyzer/Aerodynamic Particle Sizer (APS) Handbook  

SciTech Connect

The tandem differential mobility analyzer (TDMA) is a single instrument that cycles through a series of complementary measurements of the physical properties of size-resolved submicron particles. In 2008, the TDMA was augmented through the addition of an aerodynamic particle sizer (APS), which extends the upper limit of the measured size distribution into the supermicron range. These two instruments are operated in parallel, but because they are controlled by a common computer and because the size distributions measured by the two are integrated in the produced datastreams, they are described together here. Throughout the day, the TDMA sequentially measures submicron aerosol size distributions and size-resolved hygroscopic growth distributions. More specifically, the instrument is operated as a scanning DMA to measure size distributions and as a TDMA to measure size-resolved hygroscopicity. A typical measurement sequence requires roughly 45 minutes. Each morning additional measurements are made of the relative humidity (RH) dependent hygroscopicity and temperature-dependent volatility of size-resolved particles. When the outside temperature and RH are within acceptable ranges, the hydration state of size-resolved particles is also characterized. The measured aerosol distributions complement the array of aerosol instruments in the Aerosol Observing System (AOS) and provide additional details of the light-scattering and cloud-nucleating characteristics of the aerosol.

Collins, D

2010-06-18T23:59:59.000Z

255

PM2.5-Sampling and Analysis at NETL  

NLE Websites -- All DOE Office Websites (Extended Search)

PM PM 2.5 Sampling and Analysis at NETL United States Department of Energy - National Energy Technology Laboratory PM2.5rra, ST-10, 03/29/00 Why Is DOE Concerned About PM 2.5 ? * Coal-based power systems emit both primary fine particles and PM 2.5 precursors (SO 2 and NO x ) * PM 2.5 NAAQS require compliance determinations * Non-compliance will likely trigger emissions control strategies * What is the relationship between coal-fired boiler emissions and ambient PM 2.5 ? PM2.5rra, ST-10, 03/29/00 Eastern PM 2.5 Mass Apportionment - Current Understanding? 46.8% 1.1% 20.9% 3.9% 23.0% 4.3% Sulfate Nitrate Organic C Elemental C Unknown Minerals Source: EPA, April 1995 PM2.5rra, ST-10, 03/29/00 The NETL OST PM 2.5 research program has these specific research goals and objectives for FY2000: * Provide insight into the degree to which the local coal-fired electric

256

Compound class specific {sup 14}C analysis of polycyclic aromatic hydrocarbons associated with PM10 and PM1.1 aerosols from residential areas of suburban Tokyo  

SciTech Connect

Compound class specific radiocarbon analysis (CCSRA) was performed for polycyclic aromatic hydrocarbons (PAHs) associated with airborne particulate matter (APM) with diameter {lt}10 {mu}m (PM{sub 10}) and {lt}1.1 {mu}m (PM{sub 1.1}) collected from a residential area of suburban Tokyo, Japan, and seasonal and particle-size radiocarbon variations were investigated. Source diagnostic isomer pair ratios indicated mixed contributions from petroleum combustion and from biomass and coal combustion to the PAHs in APM. The {Delta}{sup 14}C-PAHs in APM, ranging from -787 to -514{per_thousand}, indicated dominance of fossil fuel combustion. The {Delta}{sup 14}C of 5-6 rings (HMW) PAHs were higher than the 3-4 rings (LMW) species in both PM{sub 10} and PM{sub 1.1} samples. The {Delta}{sup 14}C of HMW-PAHs indicated greater biomass-burning contributions in summer than in winter and no apparent particle-size variation. Conversely, the {Delta}{sup 14}C of LMW species showed a greater contribution from fossil sources in summer and in larger particles (PM10). This finding could be tentatively attributed to the recondensation of fossil-PAHs vaporized from petroleum sources. A {Delta}{sup 14}C isotopic mass balance approach estimated that biomass burning contributes 17-45% of the PAH burden in suburban Tokyo, and that the increase in the biomass-PAH accounts for approximately 27% and 22% of winter-time elevation of LMW- and HMW-PAHs, respectively. These are far exceeding what is expected from the emission statistics for CO{sub 2} and combusted materials in Japan and emphasizing the importance of biomass-burning as a source of PAHs; which, in turn, demonstrates the utility and the significance of field-based source assessment by using CCSRA for an effective regulation of atmospheric pollution by PAHs. 37 refs., 3 figs., 2 tabs.

Hidetoshi Kumata; Masao Uchida; Eisuke Sakuma; Tatsuya Uchida; Kitao Fujiwara; Mikio Tsuzuki; Minoru Yoneda; Yasuyuki Shibata [Tokyo University of Pharmacy and Life Science, Tokyo (Japan). Faculty of Life Science

2006-06-01T23:59:59.000Z

257

Different approaches to calculate the $K^{\\pm}\\to ?^{\\pm}?^0e^+e^-$ decay width  

E-Print Network (OSTI)

The rare $K^\\pm\\to\\pi^\\pm\\pi^0 e^+e^-$ decay, currently under analysis by the NA48/2 Collaboration, is considered. We have performed two theoretical approaches to calculate the differential decay width -- in the kaon rest frame, where we use Cabibbo-Maksimovicz variables, and in the center-of-mass system of the lepton pair. The latter essentially simplifies the computations. A comparison between the two approaches has been performed. We have also found the dependencies of the differential decay rate as a function of the virtual photon and dipion system masses

S. R. Gevorkyan; M. H. Misheva

2014-03-05T23:59:59.000Z

258

AUTOMATED WATER LEVEL MEASUREMENTS IN SMALL-DIAMETER AQUIFER TUBES  

SciTech Connect

Groundwater contaminated with hexavalent chromium, strontium-90, and uranium discharges into the Columbia River along approximately 16 km (10 mi) of the shoreline. Various treatment systems have and will continue to be implemented to eliminate the impact of Hanford Site contamination to the river. To optimize the various remediation strategies, it is important to understand interactions between groundwater and the surface water of the Columbia River. An automated system to record water levels in aquifer sampling tubes installed in the hyporheic zone was designed and tested to (1) gain a more complete understanding of groundwater/river water interactions based on gaining and losing conditions ofthe Columbia River, (2) record and interpret data for consistent and defensible groundwater/surface water conceptual models that may be used to better predict subsurface contaminant fate and transport, and (3) evaluate the hydrodynamic influence of extraction wells in an expanded pump-and-treat system to optimize the treatment system. A system to measure water levels in small-diameter aquifer tubes was designed and tested in the laboratory and field. The system was configured to allow manual measurements to periodically calibrate the instrument and to permit aquifer tube sampling without removing the transducer tube. Manual measurements were collected with an e-tape designed and fabricated especially for this test. Results indicate that the transducer system accurately records groundwater levels in aquifer tubes. These data are being used to refine the conceptual and numeric models to better understand interactions in the hyporheic zone of the Columbia River and the adjacent river water and groundwater, and changes in hydrochemistry relative to groundwater flux as river water recharges the aquifer and then drains back out in response to changes in the river level.

PETERSEN SW; EDRINGTON RS; MAHOOD RO; VANMIDDLESWORTH PE

2011-01-14T23:59:59.000Z

259

APIC'95, El Paso, Extended Abstracts, A Supplement to the international journal of Reliable Computing 1 Aerodynamic Aids to Vehicle Stability  

E-Print Network (OSTI)

Computing 1 Aerodynamic Aids to Vehicle Stability R. Bell Abstract--- Modern race cars utilize vari­ ous aerodynamic devices to increase stability, and traction. There is a considerable body of information available

Kreinovich, Vladik

260

Developing Supersonic Impactor and Aerodynamic Lens for Separation and Handling of Nano-Sized Particles  

SciTech Connect

A computational model for supersonic flows of compressible gases in an aerodynamic lens with several lenses and in a supersonic/hypersonic impactor was developed. Airflow conditions in the aerodynamic lens were analyzed and contour plots for variation of Mach number, velocity magnitude and pressure field in the lens were evaluated. The nano and micro-particle trajectories in the lens and their focusing and transmission efficiencies were evaluated. The computational model was then applied to design of a aerodynamic lens that could generate focus particle beams while operating under atmospheric conditions. The computational model was also applied to airflow condition in the supersonic/hypersonic impactor. Variations of airflow condition and particle trajectories in the impactor were evaluated. The simulation results could provide understanding of the performance of the supersonic and hypersonic impactors that would be helpful for the design of such systems.

Goodarz Ahmadi

2008-06-30T23:59:59.000Z

Note: This page contains sample records for the topic "aerodynamic diameter pm" from the National Library of EnergyBeta (NLEBeta).
While these samples are representative of the content of NLEBeta,
they are not comprehensive nor are they the most current set.
We encourage you to perform a real-time search of NLEBeta
to obtain the most current and comprehensive results.


261

The Formation of Systems with Tightly-packed Inner Planets (STIPs) via Aerodynamic Drift  

E-Print Network (OSTI)

The NASA Kepler mission has revealed an abundant class of Systems with Tightly-packed Inner Planets (STIPs). The current paradigm for planet formation suggests that small planetesimals will quickly spiral into the host star due to aerodynamic drag, preventing rocky planet formation. In contrast, we find that aerodynamic drift, when acting on an ensemble of solids, can concentrate mass at short orbital periods in gaseous disks. Sublimation fronts may further aid this process. Kepler data suggest that the innermost known planets are found near the silicate sublimation zone. STIP planets should have a wide range of volatile fractions due to aerodynamic drift and H2 dissociation-driven gas accretion. We further propose that the low mass of Mars is evidence that the Solar System was once a proto-STIP.

Boley, Aaron C

2013-01-01T23:59:59.000Z

262

Geodesic diameter of sets defined by few quadratic equations and inequalities  

E-Print Network (OSTI)

Geodesic diameter of sets defined by few quadratic equations and inequalities Michel Coste and Seydou Moussa September 2, 2010 Abstract We prove a bound for the geodesic diameter of a subset borrowed from D'Acunto and Kurdyka (to deal with the geodesic diameter) and from Barvinok (to take

Paris-Sud XI, Université de

263

AIAA Applied Aerodynamics Conference, 10th, Palo Alto, CA, June 22-24, 1992, Technical Papers. Pts. 1 AND 2  

SciTech Connect

Consideration is given to vortex physics and aerodynamics; supersonic/hypersonic aerodynamics; STOL/VSTOL/rotors; missile and reentry vehicle aerodynamics; CFD as applied to aircraft; unsteady aerodynamics; supersonic/hypersonic aerodynamics; low-speed/high-lift aerodynamics; airfoil/wing aerodynamics; measurement techniques; CFD-solvers/unstructured grid; airfoil/drag prediction; high angle-of-attack aerodynamics; and CFD grid methods. Particular attention is given to transonic-numerical investigation into high-angle-of-attack leading-edge vortex flow, prediction of rotor unsteady airloads using vortex filament theory, rapid synthesis for evaluating the missile maneuverability parameters, transonic calculations of wing/bodies with deflected control surfaces; the static and dynamic flow field development about a porous suction surface wing; the aircraft spoiler effects under wind shear; multipoint inverse design of an infinite cascade of airfoils, turbulence modeling for impinging jet flows; numerical investigation of tail buffet on the F-18 aircraft; the surface grid generation in a parameter space; and the flip flop nozzle extended to supersonic flows.

Not Available

1992-01-01T23:59:59.000Z

264

Missile aerodynamics; Proceedings of the Conference, Monterey, CA, Oct. 31-Nov. 2, 1988  

SciTech Connect

The present conference discusses the development status of predictive capabilities for missile aerodynamic characteristics, the application of experimental techniques to missile-release problems, prospective high-performance missile designs, the use of lateral jet controls for missile guidance, and the integration of stores on modern tactical aircraft. Also discussed are semiempirical aerodynamic methods for preliminary design, high angle-of-attack behavior for an advanced missile, and the dynamic derivatives of missiles and fighter-type configurations at high angles-of-attack.

Mendenhall, M.R.; Nixon, D.; Dillenius, M.F.E.

1989-01-01T23:59:59.000Z

265

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

E-Print Network (OSTI)

Journal of Wind Engineering and Industrial Aerodynamics, 36 (1990) 1-15 1 Elsevier the following topics: 1. 2. 3. 4. 5. 6. 7. 8. 9. 10. 11. 12. 13. Theme Lectures BluffBody Aerodynamics of Notre Dame, Notre Dame, Indiana 46556-0767; formerly, Professor and Director, Structural Aerodynamics

Kareem, Ahsan

266

To cite this document: Bechet, S. and Negulescu, C. and Chapin, Vincent and Simon, Frank Integration of CFD tools in aerodynamic design of contra-rotating  

E-Print Network (OSTI)

Integration of CFD tools in aerodynamic design of contra-rotating propellers blades. (2011) In: 3rd CEAS concerns. After a Integration of CFD Tools in Aerodynamic Design of Contra-Rotating Propeller Blades S. Béchet and C. A. Negulescu Airbus Operations S.A.S. - Aerodynamics Department, Toulouse, France V. Chapin

Mailhes, Corinne

267

The Impact of PM and HC on EGR Cooler Fouling  

Energy.gov (U.S. Department of Energy (DOE))

Data were used to correlate an EGR cooling fouling model developed to test the impact of PM and HC on fouling

268

TG-1: Portable Instrument for Transient PM Measurements | Department...  

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

Laboratory 2003deergupta.pdf More Documents & Publications High-Energy, Pulsed-Laser Diagnostics for Real-Time Measurements of Reciprocating Engine PM Emissions...

269

Thu, Sept 20, 122 pm Colloquium Speaker. "Markets, Performance, or  

E-Print Network (OSTI)

by the Department of Sociology. 4154 LSA Building. Wed, Sept 26, 4­5:30 pm Lecture. "Russia at the End of Putin

Eustice, Ryan

270

Donaldson Active Regeneration PM System | Department of Energy  

Energy.gov (U.S. Department of Energy (DOE)) Indexed Site

PM System 2005 Diesel Engine Emissions Reduction (DEER) Conference Presentations and Posters 2005deeranderson.pdf More Documents & Publications Development of an Active...

271

The California Demonstration Program for Control of PM from Diesel...  

Energy.gov (U.S. Department of Energy (DOE)) Indexed Site

for Control of PM from Diesel Backup Generators (BUGs) David R. Cocker III, Kent Johnson, John Lee, Marla Mueller, Sandip Shah, Bonnie Soriano, Bill Welch Supporting...

272

Virtual Oxygen Sensor for Innovative NOx and PM Emission Control...  

Energy.gov (U.S. Department of Energy (DOE)) Indexed Site

2009 - Poster Session August 3 rd , Hyatt Regency Dearborn Hotel Virtual Oxygen Sensor Innovative NOx and PM Emission Control Technologies J. Seebode, E. Stlting,...

273

Tuesday, 9/6 (3pm-6pm) Lobby -Counseling & Psychological Services raises awareness for Suicide Prevention Week  

E-Print Network (OSTI)

- 6:30pm) 9/19 (5:30pm - 6:30pm) FEMBA Info Session ASI Movie: Super 8 ASI Block Party Nacho Fiesta campus RefWorks user or interested in using a Bibliographic Management tool? Due to a variety of reasons or are interested in learning more about Endnote Web or Bibliographic Management tools, please feel free to let me

de Lijser, Peter

274

Estimation of unsteady aerodynamics in the wake of a freely flying European starling  

E-Print Network (OSTI)

Wing flapping is one of the most widespread propulsion methods found in nature; however, the current understanding of the aerodynamics in bird wakes is incomplete. The role of the unsteady motion in the flow and its contribution to the aerodynamics is still an open question. In the current study, the wake of a freely flying European starling has been investigated using long-duration high-speed Particle Image Velocimetry (PIV) in the near wake. Kinematic analysis of the wings and body of the bird has been performed using additional high-speed cameras that recorded the bird movement simultaneously with the PIV measurements. The wake evolution of four complete wingbeats has been characterized through reconstruction of the time resolved data, and the aerodynamics in the wake have been analyzed in terms of the streamwise forces acting on the bird. The profile drag from classical aerodynamics was found to be positive during most of the wingbeat cycle, yet kinematic images show that the bird does not decelerate. It ...

Ben-Gida, Hadar; Taylor, Zachary J; Bezner-Kerr, Wayne; Guglielmo, Christopher G; Kopp, Gregory A; Gurka, Roi

2013-01-01T23:59:59.000Z

275

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

E-Print Network (OSTI)

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 ...

Sidelko, Stephanie

2007-01-01T23:59:59.000Z

276

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

E-Print Network (OSTI)

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...

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

2004-01-01T23:59:59.000Z

277

On the Aerodynamic Performance of a Class of Vertical Shaft Windmills  

Science Journals Connector (OSTI)

...1976 research-article On the Aerodynamic Performance of a Class of Vertical Shaft Windmills P. N. Shankar A theory is presented...speed ratios corresponding to the peak power coefficient and greater. Finally, when compared with the available experimental data...

1976-01-01T23:59:59.000Z

278

Uncovering changes in spider orb-web topology owing to aerodynamic effects  

Science Journals Connector (OSTI)

...30 44 Uncovering changes in spider orb-web topology owing to aerodynamic effects Ramon...to retain prey with minimum damage to its web and at the lowest manufacturing cost. This...studies reveal that the performance of the web upon impact may not be based on the mechanical...

2014-01-01T23:59:59.000Z

279

A New Aerodynamic Traction Principle for Handling Products on an Air Cushion  

E-Print Network (OSTI)

1 A New Aerodynamic Traction Principle for Handling Products on an Air Cushion Guillaume J. Laurent. The product is carried on a thin air cushion and transported along the system by induced air flows principle for handling delicate and clean products, such as silicon wafers, glass sheets or flat foodstuff

Paris-Sud XI, Université de

280

AIAA 2002-3298 AERODYNAMICS OF TWO SIDE-BY-SIDE PLATES IN HYPERSONIC  

E-Print Network (OSTI)

AIAA 2002-3298 AERODYNAMICS OF TWO SIDE-BY-SIDE PLATES IN HYPERSONIC RAREFIED-GAS FLOWS Vladimir V. Riabov* Rivier College, Nashua, New Hampshire 03060 Abstract Hypersonic rarefied-gas flows near two side have provided valuable information related to physics of hypersonic flows about spacecraft elements

Riabov, Vladimir V.

Note: This page contains sample records for the topic "aerodynamic diameter pm" from the National Library of EnergyBeta (NLEBeta).
While these samples are representative of the content of NLEBeta,
they are not comprehensive nor are they the most current set.
We encourage you to perform a real-time search of NLEBeta
to obtain the most current and comprehensive results.


281

On the quasi-steady aerodynamics of normal hovering flight part I: the induced power factor  

Science Journals Connector (OSTI)

...Pennycuik, CJ . 2008 Modelling the flying bird. Oxford, UK: Elsevier...A Hedenstrom. 2011 Actuator disk model and span efficiency of...wingbeat kinematics in slow-flying pied flycatchers. J. R. Soc...reduce aerodynamic efficiency in flying beetles. J. R. Soc. Interface...

2014-01-01T23:59:59.000Z

282

Transition of combustion into detonation within a channel with the diameter less than the critical diameter of the existence of stationary detonation  

Science Journals Connector (OSTI)

An experimental investigation was carried out for transition of combustion into detonation of oxygen-hydrogen and hydrogen-air stoichiometric ... the critical diameter of the existence of stationary detonation in...

D. I. Baklanov; V. V. Golub; K. V. Ivanov; M. S. Krivokopytov

2012-04-01T23:59:59.000Z

283

JOURNAL DE PHYSIQUE CoZZoque C9, suppZ6ment au noll, Tome 41, novembre 1980, page C9-423 EXPERIMENTAL STUDY OF A FREE-VORTEX AERODYNAMIC WINDOW  

E-Print Network (OSTI)

-423 EXPERIMENTAL STUDY OF A FREE-VORTEX AERODYNAMIC WINDOW W. Masuda and M. Yuasa Research Institute, Ishikawajima free-vortex aerodynamic window has been fabricated and tested. Aerodynamic performance studies show of solid materials, an aerodynamic window makes use of a nonabsorbing gas jet to permit the extraction

Paris-Sud XI, Université de

284

Diameter and wall number control of carbon nanotubes by chemical vapor deposition  

SciTech Connect

We analyze the relationship between the average wall number (N) and the diameter (d) for carbon nanotubes (CNTs) grown by chemical vapour deposition. It is found that N depends linearly on d for diameters in the range of 2.5–10?nm, while single wall nanotubes predominate for diameters under about 2.1?nm. The linear relationship is found to depend somewhat on the growth conditions. It is also verified that the mean diameter depends on the diameter of the originating catalyst nanoparticle, and thus on the initial catalyst thickness where a thin film catalyst is used. This simplifies the characterisation of CNTs by electron microscopy. We also find a linear relationship between nanotube diameter and initial catalyst film thickness.

Xie, Rongsi; Zhong, Guofang, E-mail: gz222@cam.ac.uk; Zhang, Can; Chen, Bingan; Santiago Esconjauregui, C.; Robertson, John [Department of Engineering, University of Cambridge, Cambridge CB2 1PZ (United Kingdom)

2013-12-28T23:59:59.000Z

285

Demonstration abstract: PiMi air box: a cost-effective sensor for participatory indoor quality monitoring  

Science Journals Connector (OSTI)

Ultra-fine particles with aerodynamic diameter smaller than 2.5 microns, namely Particulate Matter 2.5 (PM 2.5), are capable of penetrating the lung cells and circulating the circulatory system, and compose a major health threat to people. Although the ... Keywords: cost-effective pm 2.5 sensors, indoor air quality

Linglong Li, Yixin Zheng, Lin Zhang

2014-04-01T23:59:59.000Z

286

Cost effective analysis comparing the small diameter bomb and the joint standoff weapon (A+ Variant) .  

E-Print Network (OSTI)

??This MBA project investigated and analyzed the cost effectiveness of implementing the Joint Standoff Weapon A+ (JSOW A+) variant versus the Small Diameter Bomb (SDB).… (more)

Stevens, Brett

2004-01-01T23:59:59.000Z

287

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

DOE Patents (OSTI)

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.

Steinman, D.A.

1980-05-30T23:59:59.000Z

288

Comparison of PM emissions from a gasoline direct injected (GDI) vehicle and a port fuel injected (PFI) vehicle measured by electrical low pressure impactor (ELPI) with two fuels: Gasoline and M15 methanol gasoline  

Science Journals Connector (OSTI)

Two Euro 4 gasoline passenger vehicles (one gasoline direct injected vehicle and one port fuel injected vehicle) were tested over the cold start New European Driving Cycle (NEDC). Each vehicle was respectively fueled with gasoline and M15 methanol gasoline. Particle number concentrations were measured by the electrical low pressure impactor (ELPI). Particle masses were measured by gravimetric method and estimated from the number distributions using two density distributions (one is constant with the particle size and one is power law related with the size). The first 7 stages of ELPI were used for estimation. The results show that for each vehicle, PM masses measured by gravimetric method, the total PM numbers measured by ELPI and estimated PM masses for M15 are lower than those for gasoline. For each kind of fuel, PM masses by two methods and total PM numbers from the GDI vehicle are higher than those from the PFI one. PM number distribution curves of the four vehicle/fuel combinations are similar. All decline gradually and the maximum number of each curve occurs in the first stage. More than 99.9% numbers locate in the first 8 stages of which diameters are less than 1 ?m. PM number emissions correlate well with the acceleration of the two vehicles. The estimated particle masses were much lower than the gravimetric measurements.

Bin Liang; Yunshan Ge; Jianwei Tan; Xiukun Han; Liping Gao; Lijun Hao; Wentao Ye; Peipei Dai

2013-01-01T23:59:59.000Z

289

Online PM Measurement for In-Use Testing | Department of Energy  

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

PM Measurement for In-Use Testing Online PM Measurement for In-Use Testing Modern diesel aerosol and its measurement and correlation to laboratory reference PM using the MSS 483...

290

Microsoft PowerPoint - 12 Holman White PM Conference 2010 Rev...  

Energy.gov (U.S. Department of Energy (DOE)) Indexed Site

2 Holman White PM Conference 2010 Rev 2 revised Microsoft PowerPoint - 12 Holman White PM Conference 2010 Rev 2 revised Microsoft PowerPoint - 12 Holman White PM Conference 2010...

291

Numerical simulation of aerodynamic derivatives and critical wind speed for long-span bridges based on simplified steady wind field  

Science Journals Connector (OSTI)

Combining the computational fluid dynamics-based numerical simulation with the forced vibration technique for extraction ... calculating the aerodynamic derivatives and the critical flutter wind speed for long-sp...

Dabo Xin Ph.D. Student ???; Jinping Ou ???

2007-06-01T23:59:59.000Z

292

Scramjet Operability Range Studies of an Integrated Aerodynamic-Ramp-Injector/Plasma-Torch Igniter with Hydrogen and Hydrocarbon Fuels.  

E-Print Network (OSTI)

??An integrated aerodynamic-ramp-injector/plasma-torch-igniter of original design was tested in a Mâ = 2, unvitiated, heated flow facility arranged as a diverging duct scramjet combustor. The… (more)

Bonanos, Aristides Michael

2005-01-01T23:59:59.000Z

293

Sport Days/Times Location League Options Sun: 7-11pm  

E-Print Network (OSTI)

Sport Days/Times Location League Options 3on3 Basketball Sun: 7-11pm Tue/Thu: 7-11pm Dillon Gym Courts 2 & 3 Mens, CoRec Ice Hockey Mon-Wed: 9:30-11:30pm Baker Rink Open Indoor Soccer Sun: 7-11pm Mon/Wed: 7-11pm Dillon Gym Courts 2 & 3 Mens, CoRec Wallyball Sun-Thu: 7-11pm Dillon Squash Cts Mens, Co

Singh, Jaswinder Pal

294

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

E-Print Network (OSTI)

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

Liben-Nowell, David

295

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

E-Print Network (OSTI)

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

Liben-Nowell, David

296

Instability of condensate lm and capillary blocking in small-diameter-thermosyphon condensers  

E-Print Network (OSTI)

Instability of condensate ®lm and capillary blocking in small-diameter-thermosyphon condensers H 1998 Abstract Instability of the condensate ®lm in a small-diameter-tube condenser was investigated- namic force or surface tension, the inner surface of the annular condensate ®lm is inherently unstable

Zhao, Tianshou

297

CURVATURE, DIAMETER AND BOUNDED BETTI NUMBERS Zhongmin Shen and Jyh-Yang Wu  

E-Print Network (OSTI)

CURVATURE, DIAMETER AND BOUNDED BETTI NUMBERS Zhongmin Shen and Jyh-Yang Wu Abstract. In this paper, we introduces the notion of bounded Betti numbers, and show that the bounded Betti numbers words: Diameter, Ricci curvature, sectional curvature, bounded cohomology and bounded Betti number 2000

Shen, Zhongmin

298

European Projects of Solar Diameter Monitoring Costantino Sigismondi, Michele Bianda and Jean Arnaud  

E-Print Network (OSTI)

European Projects of Solar Diameter Monitoring Costantino Sigismondi¹, Michele Bianda² and Jean Abstract. Three projects dealing with solar diameter evolution are presently in development. Historical will be monitored with fast CMOS sensors in different wavebands. The will run at IRSOL Gregory-Coudé telescope

299

Ordered Arrays of Dual-Diameter Nanopillars for Maximized Optical Absorption  

E-Print Network (OSTI)

Ordered Arrays of Dual-Diameter Nanopillars for Maximized Optical Absorption Zhiyong Fan,,,§ Rehan control to achieve the optimal absorption efficiency. Increasing the Ge materials filling ratio is shown a strong diameter dependency. To enhance the broad band optical absorption efficiency, a novel dual

Javey, Ali

300

Growth and field emission properties of small diameter carbon nanotube films  

E-Print Network (OSTI)

Growth and field emission properties of small diameter carbon nanotube films Y.Y. Wanga,*, S of the emission site intensity. D 2004 Elsevier B.V. All rights reserved. Keywords: Small diameter carbon nanotubes; MWCVD; Growth; Field emission 1. Introduction Single- or double-wall carbon nanotubes (CNT

Qin, Lu-Chang

Note: This page contains sample records for the topic "aerodynamic diameter pm" from the National Library of EnergyBeta (NLEBeta).
While these samples are representative of the content of NLEBeta,
they are not comprehensive nor are they the most current set.
We encourage you to perform a real-time search of NLEBeta
to obtain the most current and comprehensive results.


301

COLLOQUIUM - NOTE SPECIAL TIME OF 3:15PM: Savannah River National...  

NLE Websites -- All DOE Office Websites (Extended Search)

to 5:30pm Colloquia MBG Auditorium COLLOQUIUM - NOTE SPECIAL TIME OF 3:15PM: Savannah River National Laboratory: Underpinning Critical National Missions Dr. Jeff Griffin...

302

Effects of flow curvature on the aerodynamics of Darrieus wind turbines  

SciTech Connect

A theoretical and experimental investigation was conducted which clearly showed the effects of flow curvature to be significant determinants of Darrieus turbine blade aerodynamics; qualitatively, these results apply equally to straight or curved bladed machines. Unusually large boundary layer radial pressure gradients and virtually altered camber and incidence are the phenomena of primary importance. Conformal mapping techniques were developed which transform the geometric turbine airfoils in curved flow to their virtual equivalents in rectilinear flow, thereby permitting the more accurate selection of airfoil aerodynamic coefficients from published sectional data. It is demonstrated that once the flow idiosyncracies are fully understood, they may be used to advantage to improve the wind energy extraction efficiency of these machines.

Migliore, P. G.; Wolfe, W. P.

1980-07-01T23:59:59.000Z

303

A comparative study of the aerodynamics of several wind turbines using flow visualization  

SciTech Connect

This paper reports flow visualization techniques used to study the flows over the Enertech 21-5, Carter 25, and Enertech 44-50. Despite centrifugal effects superimposed on the aerodynamics, tufting (gross aerodynamic behavior) and oil flow (average boundary layer behavior), tests reveal the nature and many of the details of the flows involved. Results were compared to expected flow patterns based on angles of attack calculated from the PROPPC code. Chord Reynolds numbers ranged between 75,000 (Enertech 21-5) to 1,340,000 (Enertech 44-50). The typical low Reynolds number flow characteristics of these airfoils, including laminar separation bubbles, turbulent reattachment, and complete separation were observed. full or partial reattachment due to tower shadow was observed on each machine. Spanwise flow was observed near the leading edge of the Enertech 21-5. Cyclic radial flow from tower dam effect was also noted.

Eggleston, D.M. (Control Engineering, Univ. of Texas of the Permian Basin, Odessa, TX (US)); Starcher, K. (Alternative Energy Inst., West Texas State Univ., Canyon, TX (US))

1990-11-01T23:59:59.000Z

304

State-space model identification and feedback control of unsteady aerodynamic forces  

E-Print Network (OSTI)

Unsteady aerodynamic models are necessary to accurately simulate forces and develop feedback controllers for wings in agile motion; however, these models are often high dimensional or incompatible with modern control techniques. Recently, reduced-order unsteady aerodynamic models have been developed for a pitching and plunging airfoil by linearizing the discretized Navier-Stokes equation with lift-force output. In this work, we extend these reduced-order models to include multiple inputs (pitch, plunge, and surge) and explicit parameterization by the pitch-axis location, inspired by Theodorsen's model. Next, we investigate the na\\"{\\i}ve application of system identification techniques to input--output data and the resulting pitfalls, such as unstable or inaccurate models. Finally, robust feedback controllers are constructed based on these low-dimensional state-space models for simulations of a rigid flat plate at Reynolds number 100. Various controllers are implemented for models linearized at base angles of ...

Brunton, Steven L; Rowley, Clarence W

2014-01-01T23:59:59.000Z

305

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

E-Print Network (OSTI)

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.

Bruno, Luca

2015-01-01T23:59:59.000Z

306

Fleet Evaluation and Factory Installation of Aerodynamic Heavy Duty Truck Trailers  

SciTech Connect

The purpose of DE-EE0001552 was to develop and deploy a combination of trailer aerodynamic devices and low rolling resistance tires that reduce fuel consumption of a class 8 heavy duty tractor-trailer combination vehicle by 15%. There were 3 phases of the project: Phase 1 – Perform SAE Typed 2 track tests with multiple device combinations. Phase 2 – Conduct a fleet evaluation with selected device combination. Phase 3 – Develop the devices required to manufacture the aerodynamic trailer. All 3 phases have been completed. There is an abundance of available trailer devices on the market, and fleets and owner operators have awareness of them and are purchasing them. The products developed in conjunction with this project are at least in their second round 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).

Beck, Jason; Salari, Kambiz; Ortega, Jason; Brown, Andrea

2013-09-30T23:59:59.000Z

307

Tactical missile aerodynamics - Prediction methodology. Progress in Astronautics and Aeronautics. Vol. 142  

SciTech Connect

The present volume discusses tactical missile aerodynamic drag, drag-prediction methods for axisymmetric missile bodies, an aerodynamic heating analysis for supersonic missiles, a component buildup method for engineering analysis of missiles at low-to-high angles of attack, experimental and analytical methods for missiles with noncircular fuselages, and a vortex-cloud model for body vortex shedding and tracking. Also discussed are panel methods with vorticity effects and corrections for nonlinear compressibility, supersonic full-potential methods for missile body analysis, space-marching Euler solvers, the time-asymptotic Euler/Navier-Stokes methods for subsonic and transonic flows, 3D boundary layers on missiles, Navier-Stokes analyses of flows over slender airframes, and the interaction of exhaust plumes with missile airframes.

Mendenhall, M.R. (Nielsen Engineering and Research, Inc., Mountain View, CA (United States))

1992-01-01T23:59:59.000Z

308

Low Cost PM Technology for Particle Reinforced Titanium Automotive...  

Energy.gov (U.S. Department of Energy (DOE)) Indexed Site

Titanium Automotive Components edm2@chrysler.com February 28, 2008 Ti-6Al-4V + 10% TiC Etched Unetched RMI RMI Ti- MMC USAMP AMD 310 - Low Cost PM Technology for Particle...

309

The California Demonstration Program for Control of PM from Diesel...  

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

of PM from Diesel Backup Generators Measuring "Real World" Heavy-Duty Diesel Emissions with a Mobile Lab Emissions from In-Use NG, Propane, and Diesel Fueled Heavy Duty Vehicles...

310

The aerodynamic characteristics of an airfoil utilizing boundary layer and circulation control  

E-Print Network (OSTI)

AND DISCUSSION 22 Effects on Lift Effects on Drag 33 Effects on Pitching Moment 36 Accuracy of Data 37 Flow Interference 38 111 Chapte r VI CONCLUSIONS BIB LIO GRAPHY APPENDIX . Page 41 43 44 Table l. Aerodynamic Characteristics for Varying... control. The suction slot was 0. 065 inches wide and 2. 50 inches long in the spanwise direction. In order to measure the pressure distribution on the model, static pressure orifices were installed in the model surface at the spanwise centerline...

Boothe, Edward Milton

2012-06-07T23:59:59.000Z

311

Adaptive approach to accurate analysis of small-diameter vessels in cineangiograms  

SciTech Connect

In coronary vessels smaller than 1 mm in diameter, it is difficult to accurately identify lumen borders using existing border detection techniques. Computer-detected diameters of small coronary vessels are often severely overestimated due to the influence of the imaging system point spread function and the use of an edge operator designed for a broad range of vessel sizes. Computer-detected diameters may be corrected if a calibration curve for the X-ray system is available. Unfortunately, the performance of this postprocessing diameter correction approach is severely limited by the presence of image noise. The authors report here a new approach that uses a two-stage adaption of edge operator parameters to optimally match the edge operator to the local lumen diameter. In the first stage, approximate lumen diameters are detected using a single edge operator in a half-resolution image. Depending on the approximate lumen size, one of three edge operators is selected for the second full-resolution stage in which left and right coronary borders are simultaneously identified. The method was tested in a set of 72 segments of nine angiographic phantom vessels with diameters ranging from 0.46 to 4.14 mm and in 82 clinical coronary angiograms. Performance of the adaptive simultaneous border detection method was compared to that of a conventional border detection method and to that of a postprocessing diameter correction border detection method. Adaptive border detection yielded significantly improved accuracy in small phantom vessels and across all vessel sizes in comparison to the conventional and postprocessing diameter correction methods. Adaptive simultaneous coronary border detection provides both accurate and robust quantitative analysis of coronary vessels of all sizes.

Sonka, M.; Winniford, M.D.; Collins, S.M. [Univ. of Iowa, Iowa City, IA (United States)] [Univ. of Iowa, Iowa City, IA (United States); Reddy, G.K. [Cemax-Icon, Inc., Fremont, CA (United States)] [Cemax-Icon, Inc., Fremont, CA (United States)

1997-02-01T23:59:59.000Z

312

Hydrodynamic Model with Binary Particle Diameters to Predict Axial Voidage Profile in a CFB Combustor  

Science Journals Connector (OSTI)

A hydrodynamic model with binary particle diameters was developed to better predict axial voidage profile in a CFB combustor. In the model, the CFB is regarded as a superposition of two ... field data of voidage ...

J. J. Li; H. Zhang; H. R. Yang; Y. X. Wu…

2010-01-01T23:59:59.000Z

313

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

E-Print Network (OSTI)

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) pressurizer surge line...

Williams, Susan Nicole

2010-10-12T23:59:59.000Z

314

Effects of CSP Support Particle Size on the Performance of Larger Diameter Liquid Partition Columns  

Science Journals Connector (OSTI)

......research-article Editorial Effects of CSP Support Particle Size on the Performance...packed with different particle sizes of CSP (controlled surface porosity) support...larger, infinite-diameter columns and CSP support used in this study. Reduced plate......

H. C. Beachell; J. J. DeStefano

1972-08-01T23:59:59.000Z

315

Yb-doped Large Pitch Fiber with 105µm Mode Field Diameter  

Science Journals Connector (OSTI)

We present an active Yb-doped Large Pitch Fiber with 105µm mode field diameter. It was tested in a fiber CPA system delivering <500fs, 2mJ pulses with 3.8GW peak power. The...

Jansen, Florian; Stutzki, Fabian; Eidam, Tino; Rothhardt, Jan; Hädrich, Steffen; Carstens, Henning; Jauregui, Cesar; Limpert, Jens; Tünnermann, Andreas

316

IMPACT STRUCTURES: WHAT DOES CRATER DIAMETER MEAN? E. P. Turtle1,2 , E. Pierazzo2  

E-Print Network (OSTI)

IMPACT STRUCTURES: WHAT DOES CRATER DIAMETER MEAN? E. P. Turtle1,2 , E. Pierazzo2 , G. S. Collins1 and Planetary Lab., Univ. of Arizona, Tucson, AZ 85721-0092; turtle@lpl.arizona.edu, 2 Planetary Science Inst

Collins, Gareth

317

Friday . . . . . . . . . . . . . . October 31, 2014 noon -5 pm Registration and poster setup  

E-Print Network (OSTI)

PROGRAM Friday . . . . . . . . . . . . . . October 31, 2014 noon - 5 pm Registration and poster setup 3 - 5 pm Informal poster viewing 6 - 7 pm Reception 7 - 9 pm Welcoming Banquet & Speaker Saturday of a Symposium featur- ing poster and oral presentations by students and graduate trainees participating

Cui, Yan

318

August 22 Marc Mignolet Welcome 1:30 pm Arizona State University  

E-Print Network (OSTI)

"Self Sustaining Turbulence in Restricted Nonlinear 1:30 pm Johns Hopkins University Model" Location

319

Wed. 9 October '13 at 7.00 pm Reception, Room 253, Gilbert Scott Building  

E-Print Network (OSTI)

Kelvingrove Art Gallery Christmas lunch Mon. 20 January '14 at 7.15 pm for 7.30 pm Eric Flack Garscadden April '14 at 7.15 pm for 7.30 pm Joy Blair #12;Sea Lights Thurs. 15 May '14, 9.15 am for 9.30am, Boyd

Glasgow, University of

320

E-Print Network 3.0 - aerodynamic particle interaction Sample...  

NLE Websites -- All DOE Office Websites (Extended Search)

time scale... diameter particles are actually more likely to interact with the evaporator tube walls than the small... , rather than relying entirely on heat transfer from the...

Note: This page contains sample records for the topic "aerodynamic diameter pm" from the National Library of EnergyBeta (NLEBeta).
While these samples are representative of the content of NLEBeta,
they are not comprehensive nor are they the most current set.
We encourage you to perform a real-time search of NLEBeta
to obtain the most current and comprehensive results.


321

Modular PM Motor Drives for Automotive Traction Applications  

SciTech Connect

This paper presents modular permanent magnet (PM) motor drives for automotive traction applications. A partially modularized drive system consisting of a single PM motor and multiple inverters is described. The motor has multiple three-phase stator winding sets and each winding set is driven with a separate three-phase inverter module. A truly modularized inverter and motor configuration based on an axial-gap PM motor is then introduced, in which identical PM motor modules are mounted on a common shaft and each motor module is powered by a separate inverter module. The advantages of the modular approach for both inverter and motor include: (1) power rating scalability--one design meets different power requirements by simply stacking an adequate number of modules, thus avoiding redesigning and reducing the development cost, (2) increased fault tolerance, and (3) easy repairing. A prototype was constructed by using two inverters and an axial-gap PM motor with two sets of three-phase stat or windings, and it is used to assist the diesel engine in a hybrid electric vehicle converted from a Chevrolet Suburban. The effect of different pulse-width-modulation strategies for both motoring and regenerative modes on current control is analyzed. Torque and regenerative control algorithms are implemented with a digital signal processor. Analytical and initial testing results are included in the paper.

Su, G.J.

2001-10-29T23:59:59.000Z

322

Aerodynamic characteristics of seven symmetrical airfoil sections through 180-degree angle of attack for use in aerodynamic analysis of vertical axis wind turbines  

SciTech Connect

When work began on the Darrieus vertical axis wind turbine (VAWT) program at Sandia National Laboratories, it was recognized that there was a paucity of symmetrical airfoil data needed to describe the aerodynamics of turbine blades. Curved-bladed Darrieus turbines operate at local Reynolds numbers (Re) and angles of attack (..cap alpha..) seldom encountered in aeronautical applications. This report describes (1) a wind tunnel test series conducted at moderate values of Re in which 0 less than or equal to ..cap alpha.. less than or equal to 180/sup 0/ force and moment data were obtained for four symmetrical blade-candidate airfoil sections (NACA-0009, -0012, -0012H, and -0015), and (2) how an airfoil property synthesizer code can be used to extend the measured properties to arbitrary values of Re (10/sup 4/ less than or equal to Re less than or equal to 10/sup 7/) and to certain other section profiles (NACA-0018, -0021, -0025).

Sheldahl, R E; Klimas, P C

1981-03-01T23:59:59.000Z

323

Hillman Library 10 a.m.6 p.m. closed Falk Library (HSLS) 9:30 a.m.10 p.m. closed  

E-Print Network (OSTI)

Library Saturday may 24 Sunday may 25 monday may 26 Hillman Library 10 a.m.­6 p.m. closed Falk Library (HSLS) 9:30 a.m.­10 p.m. closed Barco Law Library 9 a.m.­5 p.m. closed Stark Media Services noon­5 p.m. closed Archives Service Center Business Library Chemistry Library Bevier Engineering Library

Jiang, Huiqiang

324

Initial Takeaways from the PM Workshop | OpenEI Community  

Open Energy Info (EERE)

Initial Takeaways from the PM Workshop Initial Takeaways from the PM Workshop Home > Groups > EERE - Energy Data Initiative Ianjkalin's picture Submitted by Ianjkalin(84) Contributor 14 July, 2012 - 12:00 Thanks again to everyone who participated in the PM Workshop. Here are the top ideas, action items and datasets that we all collectively determined to be most important: Top "Big Ideas" A. Create, implement and then develop skills / tools to execute Programs with more of a "Customer Centric" approach to Data. B. Utilize a "reverse auction" approach in order to drive down costs for early-stage company adoption. C. Integrate potential of Data into R&D planning process. D. Improve integration of electric and gas generation assets during the (oftentimes long) comissioning periods.

325

AMBIENT PM2.5 SAMPLING AND ANALYSIS  

SciTech Connect

This interim report summarizes detailed findings and conclusions drawn from evaluations of data obtained from the operation of ambient PM{sub 2.5} speciation sites in a geographical area encompassing southeastern Ohio, western Pennsylvania and northwestern West Virginia. The overall goal of this program, called the Upper Ohio River Valley Project (UORVP), is to better understand the relationship between coal-based power system emissions and ambient air quality in the Upper Ohio River Valley region through the collection of chemically resolved or speciated data. A summary of the sampling activities, sample analyses and the correlation and interpretation of data acquired from February 1999 through March of 2001 are reported. Mass and speciated data from urban and rural sources are compared and seasonal variations in PM{sub 2.5} distribution are also examined. Correlations between meteorological parameters and total PM{sub 2.5} mass are also presented.

Unknown

2002-10-31T23:59:59.000Z

326

AMBIENT PM2.5 SAMPLING AND ANALYSIS  

SciTech Connect

This interim report summarizes detailed findings and conclusions drawn from evaluations of data obtained from the operation of ambient PM{sub 2.5} speciation sites in a geographical area encompassing southeastern Ohio, western Pennsylvania and northwestern West Virginia. The overall goal of this program, called the Upper Ohio River Valley Project (UORVP), is to better understand the relationship between coal-based power system emissions and ambient air quality in the Upper Ohio River Valley region through the collection of chemically resolved or speciated data. A summary of the sampling activities, sample analyses and the correlation and interpretation of data acquired from February 1999 through March of 2001 are reported. Mass and speciated data from urban and rural sources are compared and seasonal variations in PM{sub 2.5} distribution are also examined. Correlations between meteorological parameters and total PM{sub 2.5} mass are also presented.

Unknown

2001-10-31T23:59:59.000Z

327

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

E-Print Network (OSTI)

VARIATION IN THE AERODXMMIC DRAG COEEEICIENT DUE TO CHANGES LN THE SHAPE OF AN AUTOMOBILE A Thesis by JOHN GILBERT MILLI%MS Su'bmitned to the Graduate College of the Texas A&M University in partial fulfillment of the requirements fo... Air Density C HAFTER I IliiTRODUCTION During the early years of the automobile, little or no effort was made to explore the problem of aerodynamic drag. This situation was the result oi' two factors. First, the passenger cars of shat time were...

Williams, John Gilbert

1968-01-01T23:59:59.000Z

328

Numerical computation of aerodynamic sensitivity coefficients in the transonic and supersonic regimes  

E-Print Network (OSTI)

). Differentiating Eqs. (9) and (10) with respect to x and substituting the results into Eq. (8) yields For parabolic-arc sections Fu 1 - 2C(L-x)/LL ? w + 2T(1-2x) For NACA four-digit sections (11) Fu 1 - 2C(L-x)/LL + 5T(0. 14845/Jx-0. 126-0. 7032x+0. 8529x... by Leland A. Garison (Chair of Committee) Cyrus Ostowari (Member) Steven D. Talia erro (Member) W. E. Haisler (Head of Department) May 1988 ABSTRACT Numerical Computation of Aerodynamic Sensitivity Coefficients in the Transonic and Supersonic...

Elbanna, Hesham Mahmoud

1988-01-01T23:59:59.000Z

329

Aerodynamic Thrust Modelling in Wave Tank Tests of Offshore Floating Wind Turbines Using a Ducted Fan  

Science Journals Connector (OSTI)

Wave tank testing of scaled models is standard practice during the development of floating wind turbine platforms for the validation of the dynamics of conceptual designs. Reliable recreation of the dynamics of a full scale floating wind turbine by a scaled model in a basin requires the precise scaling of the masses and inertias and also the relevant forces and its frequencies acting on the system. The scaling of floating wind turbines based on the Froude number is customary for basin experiments. This method preserves the hydrodynamic similitude, but the resulting Reynolds number is much lower than in full scale. The aerodynamic loads on the rotor are therefore out of scale. Several approaches have been taken to deal with this issue, like using a tuned drag disk or redesigning the scaled rotor. This paper describes the implementation of an alternative method based on the use of a ducted fan located at the model tower top in the place of the rotor. The fan can introduce a variable force that represents the total wind thrust by the rotor. A system controls this force by varying the rpm, and a computer simulation of the full scale rotor provides the desired thrust to be introduced by the fan. This simulation considers the wind turbine control, gusts, turbulent wind, etc. The simulation is performed in synchronicity with the test and it is fed in real time by the displacements and velocities of the platform captured by the acquisition system. Thus, the simulation considers the displacements of the rotor within the wind field and the calculated thrust models the effect of the aerodynamic damping. The system is not able currently to match the effect of gyroscopic momentum. The method has been applied during a test campaign of a semisubmersible platform with full catenary mooring lines for a 6MW wind turbine in scale 1/40 at Ecole Centrale de Nantes. Several tests including pitch free decay under constant wind and combined wave and wind cases have been performed. Data from the experiments are compared with aero-servo-hydro-elastic computations with good agreement showing the validity of the method for the representation of the scaled aerodynamics. The new method for the aerodynamic thrust scaling in basin tests is very promising considering its performance, versatility and lower cost in comparison with other methods.

José Azcona; Faisal Bouchotrouch; Marta González; Joseba Garciandía; Xabier Munduate; Felix Kelberlau; Tor A Nygaard

2014-01-01T23:59:59.000Z

330

Tactical missile aerodynamics - General topics. Progress in Astronautics and Aeronautics. Vol. 141  

SciTech Connect

The present volume discusses the development history of tactical missile airframes, aerodynamic considerations for autopilot design, a systematic method for tactical missile design, the character and reduction of missile observability by radar, the visualization of high angle-of-attack flow phenomena, and the behavior of low aspect ratio wings at high angles of attack. Also discussed are airbreathing missile inlets, 'waverider' missile configurations, bodies with noncircular cross-sections and bank-to-turn missiles, asymmetric flow separation and vortex shedding on bodies-of-revolution, unsteady missile flows, swept shock-wave/boundary-layer interactions, pylon carriage and separation of stores, and internal stores carriage and separation.

Hemsch, M.J. (Lockheed Engineering and Sciences Co., Hampton, VA (United States))

1992-01-01T23:59:59.000Z

331

Economic and Performance Benefits Resulting From the Use of Large Diameter  

Open Energy Info (EERE)

and Performance Benefits Resulting From the Use of Large Diameter and Performance Benefits Resulting From the Use of Large Diameter Fans on Air Cooled Heat Exchangers (A Case Study in the Use of Large Fan Air Cooled Condensers at the Neal Hot Springs Geothermal Power Plant, Oregon) Jump to: navigation, search OpenEI Reference LibraryAdd to library Journal Article: Economic and Performance Benefits Resulting From the Use of Large Diameter Fans on Air Cooled Heat Exchangers (A Case Study in the Use of Large Fan Air Cooled Condensers at the Neal Hot Springs Geothermal Power Plant, Oregon) Abstract A significant improvement in air cooler technology was implementedat the Neal Hot Springs geothermal power plant in Vale,Oregon. Large cooling tower fans were used in an induced draftarrangement (fans above the heat exchanger). The total numberof fans was reduced from 270 x 12ft / 3.7m fans

332

Plugging nuclear waste pipelines: impact of high level waste slurry characteristics and pipe diameter  

SciTech Connect

The work presented here focuses on experiments carried out in 22-mm ID and 45-mm ID pipelines utilizing slurries composed of spherical glass beads having particle size distribution following the Rosin-Rammler distribution and mean size of 50 {mu}m. The spreads of the distribution were 1.7 and 7, corresponding to wide and narrow distributions, respectively. The slurries utilized in this study had concentrations ranging from 5% to 25% by volume. Results obtained in the same pipeline diameter indicated that the slurry of the narrower distribution experienced higher pressure drops and lower critical deposition velocities than those for the slurry of wider distribution. Pressure drop increased markedly with increasing slurry concentration regardless of the pipe diameter and slurry PSD. However, the pipe diameter was found to have more significant influence on the pressure drop than the slurry concentration does. (authors)

Daas, M.; Srivastava, R.; Skudarnov, P. [Florida International Univ., Applied Research Center, Miami, FL (United States)

2007-07-01T23:59:59.000Z

333

BusinessandManagement extension.uci.edu/pm  

E-Print Network (OSTI)

project managers, and those who want to make a career transition into project management. Upon completionBusinessandManagement extension.uci.edu/pm CHARTER MEMBER ® Project Management Institute REP#1043 Project Management Certificate Program Accelerate Your Career The PMI Registered Education Provider logo

Rose, Michael R.

334

Performance of a High Volume PM2.5 Sampler  

E-Print Network (OSTI)

.5) concentrations can be measured by a Federal Equivalent Method (FEM) sampler. Environmental Protection Agency (EPA) designates PM_(2.5) samplers which meet the requirements specified in 40 Code of Federal Regulation (CFR), Part 53, Subpart F as FEM samplers...

Li, Huan

2013-12-12T23:59:59.000Z

335

A Peltier cooling system for SiPM temperature stabilization  

E-Print Network (OSTI)

A Peltier cooling system for SiPM temperature stabilization von Simon Nieswand Bachelorarbeit auÃ?en thermisch isolierten Kupferblockes einzulassen, an welchen ein Peltier-Element angebracht wird. Um das System zu automatisieren, werden der Temperatursensor und die Stromquelle des Peltier- Elements

Hebbeker, Thomas

336

Thursday October 10 7:30 pm Rockefeller Chapel  

E-Print Network (OSTI)

A celebration of Swami Vivekananda on the 150th anniversary of his birth, with the lighting of one hundred. diwali: The indian feSTival of lighTS Friday November 1 5:30 pm Rockefeller A traditional Diwali puja in partnership with the Greater Chicago Food Depository. RSVP spirit@uchicago.edu. ChRiSTMaS ORaTORiO Sunday

He, Chuan

337

WWU Sustainability Academy 4PM, Wednesday, December 3, CF 125  

E-Print Network (OSTI)

WWU Sustainability Academy 4PM, Wednesday, December 3, CF 125 Draft Agenda 1. Welcome ­ Facilitators panel 2. Establishing a WWU Sustainability Academy Responses to Survey Questionnaire What the WWU Sustainability Academy can do Advocating for sustainability studies at WWU 3. The Existing

Zaferatos, Nicholas C.

338

WWU Sustainability Academy 4PM, Wednesday, December 3, CF 125  

E-Print Network (OSTI)

WWU Sustainability Academy 4PM, Wednesday, December 3, CF 125 Agenda 1. WWU Sustainability Academy Sustainability Courses at WWU ­ Gene Myers 4. Existing Sustainability Prototype Programs at WWU ­ Arunas Oslapas faculty member in the Sustainability Academy · 25 Yes · 6 Not sure Anonymous surveyors: · 7 Not sure · 1

Zaferatos, Nicholas C.

339

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

SciTech Connect

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.

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

2014-06-01T23:59:59.000Z

340

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

SciTech Connect

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.

Robert J. Englar

2001-05-14T23:59:59.000Z

Note: This page contains sample records for the topic "aerodynamic diameter pm" from the National Library of EnergyBeta (NLEBeta).
While these samples are representative of the content of NLEBeta,
they are not comprehensive nor are they the most current set.
We encourage you to perform a real-time search of NLEBeta
to obtain the most current and comprehensive results.


341

Aerodynamic efficiency of smoke ventilators in light streets and shed-type roofs  

Science Journals Connector (OSTI)

Low-rise industrial buildings in continental Europe have usually no or very little window area in the sidewalls. To provide the necessary daylight, translucent surfaces are fitted in the roof. Well known examples are shed roofs or curved and shed-type light streets in flat roofs. For economic reasons smoke ventilators are then integrated into the light surfaces. This paper gives typical examples of smoke ventilators installed in shed roofs and in curved or shed-type light streets. The measurement of the aerodynamic free areas on full scale apparatus is not possible due to the large dimensions of the relevant roof surfaces. Therefore, tests have to be conducted in model scale. The relevant similarity considerations for such model tests are discussed and the applicability of model scale tests is demonstrated. Finally, the most important parameters influencing the aerodynamic efficiency of typical ventilator installations in shed-roofs and curved or shed-type light streets are described for the cases without and with side wind.

H.J. Gerhardt; C. Kramer

1993-01-01T23:59:59.000Z

342

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)

://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, University of Michigan, Ann Arbor, MI Abstract Despite considerable research on aerodynamic shape

Papalambros, Panos

343

The development of the quality assurance program for PM2.5: The December 13, 1996 proposal, the July 18, 1997 regulations and the public comments concerning QA  

SciTech Connect

The Environmental Protection Agency (EPA) has developed a new National Ambient Air Quality Standard (NAAQS) standard for particles in the atmosphere with aerometric diameters of 2.5 micrometers or less. The EPA has also promulgated a new federal reference and equivalent method program to regulate the methods needed to monitor these particles. This federal reference method (FRM) is very complex and sensitive and requires enhanced quality assurance (QA) and quality control (QC) procedures to ensure that a valid sample is collected. The QA program for PM2.5 was first introduced in the December 13, 1996 proposal published in the Federal Register. This proposal outlined several QA procedures for the PM2.5 program. The precision of an existing monitoring network was to be determined with collocated monitors and flow checks. The bias of a monitoring network was to be determined with a new QA procedure that required bi-monthly audits on all PM2.5 monitors using a portable FRM audit sampler. Consistent with Agency policy, this proposal was open to public comment and review. The Agency received over 30,000 comments many of which concerned the QA program. The QA system was modified, based upon these comments, to reduce the logistical burden for the implementation of the program. The subsequent modifications were finalized in the July 18, 1997 regulations published in the Federal Register. This finalized QA program required 25% of the monitors to be collocated, quarterly flow audits on all PM2.5 monitors used in the SLAMS network, and 25% of all PM2.5 monitors to be independently audited with the new FRM audit sampler. Details of the QA system are found in 40 CFR Part 58, Appendix A.

Musick, D.; Papp, M.; Elkins, J. [Environmental Protection Agency (United States)

1998-12-31T23:59:59.000Z

344

Ping Liu PhD FRIDAY, FEB. 8, 2013 3:30PM to 4:30PM  

E-Print Network (OSTI)

electrification and grid storage, two large-scale applications essential for realizing a sustainable energy future Before Seminar at 3:10PM in Room 113 Challenges and Opportunities for Long Life Energy Storage conversion and storage. Dr. Liu was previously Manager of Energy Technology at HRL Laboratories

345

Predicting Primary PM2.5 and PM0.1 Trace Composition for Epidemiological Studies in California  

Science Journals Connector (OSTI)

§ Atmospheric Chemistry Division, National Center for Atmospheric Research, Boulder, Colorado ... High resolution emissions from wildfires and open burning (1 × 1 km)(-58, 59) were included in this study, but emissions of biogenic particles and sea-salt particles were not included. ... Wildfire dominates the contributions to all primary PM components in areas near the fires. ...

Jianlin Hu; Hongliang Zhang; Shu-Hua Chen; Christine Wiedinmyer; Francois Vandenberghe; Qi Ying; Michael J. Kleeman

2014-04-02T23:59:59.000Z

346

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

DOE Patents (OSTI)

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.

Hauge, Robert H; Xu, Ya-Qiong

2013-08-13T23:59:59.000Z

347

Carbon nanotube diameter selection by pretreatment of metal catalysts on surfaces  

DOE Patents (OSTI)

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.

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)

2012-02-28T23:59:59.000Z

348

THE DIAMETER OF THE ISOMORPHISM CLASS OF A BANACH W. B. JOHNSON AND E. ODELL  

E-Print Network (OSTI)

THE DIAMETER OF THE ISOMORPHISM CLASS OF A BANACH SPACE W. B. JOHNSON AND E. ODELL August 20, 2004 is finitely complementably universal; that is, there is Johnson was supported in part by NSF DMS­0200690 and Probability at Texas A&M University. MR subject classification: 46G05, 46T20. 1 #12; 2 W. B. JOHNSON AND E

Johnson, William B.

349

Phenomenological modeling of tumor diameter growth based on a mixed effects  

E-Print Network (OSTI)

Phenomenological modeling of tumor diameter growth based on a mixed effects model T. Bastogne a,, A tumor volume-based models have been devel- oped for the phenomenological modeling of tumor growth-00390380,version1-2Jun2009 #12;1 Introduction In systems theory1,2 , phenomenological or black-box models

Boyer, Edmond

350

High-Yield Sorting of Small-Diameter Carbon Nanotubes for Solar Cells and Transistors  

Science Journals Connector (OSTI)

High-Yield Sorting of Small-Diameter Carbon Nanotubes for Solar Cells and Transistors ... G.I.K. acknowledges the support of the Government of Canada and the Natural Sciences and Engineering Research Council of Canada (NSERC) in the form of the Banting Postdoctoral Fellowship. ...

Huiliang Wang; Ghada I. Koleilat; Peng Liu; Gonzalo Jiménez-Osés; Ying-Chih Lai; Michael Vosgueritchian; Ya Fang; Steve Park; Kendall N. Houk; Zhenan Bao

2014-01-31T23:59:59.000Z

351

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

E-Print Network (OSTI)

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 electron emitter. By adjusting the catalytic synthesis conditions, single-walled carbon nanotubes (SWNT

Resasco, Daniel

352

E-Print Network 3.0 - airborne particles pm10 Sample Search Results  

NLE Websites -- All DOE Office Websites (Extended Search)

<< < 1 2 3 4 5 > >> 1 Correlating Bioaerosol Load with PM2.5 and PM10 Concentrations Jordan Peccia1, Ann M. Dillner1,2, Justin Boreson1 Summary: exposure of airborne biological...

353

Development of methodology to correct sampling error associated with FRM PM10 samplers  

E-Print Network (OSTI)

Currently, a lack of accurate emission data exits for particulate matter (PM) in agricultural air quality studies (USDA-AAQTF, 2000). PM samplers, however, tend to over estimate the concentration of most agricultural dusts because of the interaction...

Chen, Jing

2009-05-15T23:59:59.000Z

354

DSM-PM2: A Portable Implementation Platform for Multithreaded DSM Consistency Protocols  

Science Journals Connector (OSTI)

DSM-PM2 is a platform for designing, implementing and experimenting with multithreaded DSM consistency protocols. It provides a generic toolbox ... alternative protocols for a given consistency model. DSM-PM2 is ...

Gabriel Antoniu; Luc Bougé

2001-01-01T23:59:59.000Z

355

January 13, 2010, 3 p.m. Susan Hackwood and Jeffrey Rudolph  

E-Print Network (OSTI)

RightinanImperfectWorld:CatalyzingtheFuture April 5, 2010, 3 p.m. Bhakta Rath Naval Research Laboratory EnergyAfterOil April 15, 2010, 3 p.m. Mary

356

Reflecting the Revised PM 2.5 National Ambient Air Quality Standard...  

Energy.gov (U.S. Department of Energy (DOE)) Indexed Site

Reflecting the Revised PM 2.5 National Ambient Air Quality Standard in NEPA Evaluations Reflecting the Revised PM 2.5 National Ambient Air Quality Standard in NEPA Evaluations This...

357

A study on aerodynamics and mechanisms of elementary morphing models for flapping wing in bat forward flight  

E-Print Network (OSTI)

The large active wing deformation is a significant way to generate high aerodynamic forces required in bat flapping flight. Besides the twisting, the elementary morphing models of a bat wing are proposed, such as wing-bending in the spanwise direction, wing-cambering in the chordwise direction, and wing area-changing. A plate of aspect ratio 3 is used to model a bat wing and a three dimensional unsteady panel method is applied to predict the aerodynamic forces. It is found that the cambering model has a great positive influence on the lift, followed by area-changing model and then the bending model. The further study indicates that the vortex control is a main mechanism to produce high aerodynamic forces, and the mechanisms for the aerodynamic force enhancement are the asymmetry of the cambered wing and the amplifier effects of wing area-changing and wing bending. The lift and thrust are mainly generated during the downstroke and almost negligible forces during the upstroke by the integrated morphing model-wi...

Zi-Wu, Guan

2014-01-01T23:59:59.000Z

358

Plant Pathology (Geneva) Seminars FALL 2013 All Seminars--3:30 PM (Coffee @ 3:00)  

E-Print Network (OSTI)

, fruit composition, and leaching of agrochemicals in a Finger Lakes vineyard December 4 12:20 PM Bruce Mc

Lazzaro, Brian

359

Library Monday -Thursday Friday Saturday Lied Library 7:30 a.m. -Midnight 7:30 a.m. -7 p.m. 9 a.m. -6 p.m.  

E-Print Network (OSTI)

Library Monday - Thursday Friday Saturday Lied Library 7:30 a.m. - Midnight 7:30 a.m. - 7 p.m. 9 a.m. - 6 p.m. Lied Library - Special Collections 9 a.m. - 7 p.m. 9 a.m. - 5 p.m. Closed Architecture Studies Library (ASL) 9 a.m. - 9 p.m. 9 a.m. - 5 p.m. Closed Curriculum Materials Library (CML) 8 a.m. - 8

Hemmers, Oliver

360

Fractional-slot PM motors for electric power steering systems  

Science Journals Connector (OSTI)

This paper deals with some considerations about a PM motor with fractional number of slot per pole per phase, adopted for an electric power steering system. The key requirements of such a system, such as efficiency, torque ripple, fault tolerance, weight and cost, are considered and discussed. The possibility to design the motor in different forms is investigated, introducing some criteria to evaluate the convenience of using non-overlapping winding.

N. Bianchi; S. Bolognani

2004-01-01T23:59:59.000Z

Note: This page contains sample records for the topic "aerodynamic diameter pm" from the National Library of EnergyBeta (NLEBeta).
While these samples are representative of the content of NLEBeta,
they are not comprehensive nor are they the most current set.
We encourage you to perform a real-time search of NLEBeta
to obtain the most current and comprehensive results.


361

Aerodynamic drag reduction apparatus for gap-divided bluff bodies such as tractor-trailers  

DOE Patents (OSTI)

An apparatus for reducing the aerodynamic drag of a bluff-bodied vehicle such as a tractor-trailer in a flowstream, the bluff-bodied vehicle of a type having a leading portion, a trailing portion connected to the leading portion, and a gap between the leading and trailing portions defining a recirculation zone. The apparatus is preferably a baffle assembly, such as a vertical panel, adapted to span a width of the gap between the leading and trailing portions so as to impede cross-flow through the gap, with the span of the baffle assembly automatically adjusting for variations in the gap width when the leading and trailing portions pivot relative to each other.

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

2006-07-11T23:59:59.000Z

362

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

SciTech Connect

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.

Xu, Tengfang; Jeng, Ming-Shan

2004-07-27T23:59:59.000Z

363

Investigation of Tractor Base Bleeding for Heavy Vehicle Aerodynamic Drag Reduction  

SciTech Connect

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.

Ortega, J; Salari, K; Storms, B

2007-10-25T23:59:59.000Z

364

Results from dynamic tests and analyses of a medium diameter LMFBR piping system  

SciTech Connect

This paper presents results and observations from dynamic tests and analyses performed on a 0.20 m (8 in.) diameter, thin walled piping system. The piping system is a scaled representation of a Liquid Metal Fast Breeder Reactor (LMFBR) large diameter piping loop. Prototypic piping restraints were employed, including mechanical snubbers, rigid struts, pipe hangers and non-integral pipe clamps. Snapback, sine-sweep and seismic tests were performed for various restraint configurations and piping conditions. The test results are compared to analytical predictions for verification of the methods and models used in the seismic design of LMFBR piping systems. Test program conclusions and general recommendations for piping seismic analyses are presented along with a discussion of test and analysis results.

Schott, G.A.; Heberling, C.F.; Hulbert, G.M.

1984-06-01T23:59:59.000Z

365

Results from dynamic tests and analyses of a medium diameter LMFBR piping system  

SciTech Connect

This paper presents results and observations from dynamic tests and analyses performed on an 8-in. (0.20-m) diameter, thin-walled piping system. The piping system is a scaled representation of a Liquid Metal Fast Breeder Reactor (LMFBR) large diameter piping loop. Prototypic piping restraints were employed, including mechanical snubbers, rigid struts, pipe hangers and nonintegral pipe clamps. Snapback, sine-sweep and seismic tests were performed for various restraint configurations and piping conditions. The test results are compared to analytical predictions for verification of the methods and models used in the seismic design of LMFBR piping systems. Test program conclusions and general recommendations for piping seismic analyses are presented along with a discussion of test and analysis results.

Schott, G.A.; Hulbert, G.M.; Heberling, C.F. II

1986-08-01T23:59:59.000Z

366

Cosmic equation of state from combined angular diameter distances: Does the tension with luminosity distances exist?  

E-Print Network (OSTI)

Using a relatively complete observational data concerning four angular diameter distance (ADD) measurements and %synthetic combined SN+GRB observations representing current luminosity distance (LD) data, this paper investigates the %tension between compatibility of these two cosmological distances considering three classes of dark energy equation of state (EoS) reconstruction. In particular, we use strongly gravitationally lensed systems from various large systematic gravitational lens surveys and galaxy clusters, which yield the Hubble constant independent ratio between two angular diameter distances $D_{ls}/D_s$ data. Our results demonstrate that, with more general categories of standard ruler data, ADD and LD data are compatible at $1\\sigma$ level. Secondly, we note that consistency between ADD and LD data %are blind is maintained irrespective of the EoS parameterizations: there is a good match between the universally explored CPL model and other formulations of cosmic equation of state. Especially for the...

Cao, Shuo

2014-01-01T23:59:59.000Z

367

Diameters of Single-Wall Carbon Nanotubes Depending on Helium Gas Pressure in an Arc Discharge  

Science Journals Connector (OSTI)

Diameters of Single-Wall Carbon Nanotubes Depending on Helium Gas Pressure in an Arc Discharge ... So far, relatively large quantities of SWNTs have been produced by using Y?Ni and Fe?Ni catalysts for the electric arc discharge method28-30 and by using a Co?Ni catalyst for the pulsed laser ablation method. ... The electric current of the arc discharge also affected the yield of SWNTs though its effect was not as serious as the helium pressure. ...

Yahachi Saito; Yoshihiko Tani; Atsuo Kasuya

2000-02-26T23:59:59.000Z

368

24th AIAA Applied Aerodynamics Conference, Jun. 5-8, 2006, San Francisco, CA Flight Control of a UAV with Inflatable Wings with  

E-Print Network (OSTI)

24th AIAA Applied Aerodynamics Conference, Jun. 5-8, 2006, San Francisco, CA Flight Control are conceptually possible in almost any size and have been developed with spans as small as 6 inches for missiles

Jacob, Jamey

369

2014 8 22 4:00PM-5:00PM Title: "Exploration of the Higgs boson and the Physics case for the Large Hadron Electron  

E-Print Network (OSTI)

2014 8 22 4:00PM-5:00PM Title: "Exploration of the Higgs boson and the Physics case for the Large Hadron Electron Collider" Abstract: With the discovery of a Higgs boson at the Large Hadron) Prof. Mellado is an expert on the Higgs boson ­ a sub-atomic particle that is thought to give matter

Wang, Yayu

370

11/30/2006 -3:00 pm -4:30 pm Room:San Polo -3404 (ISD Campus) Autodesk MapGuide Techniques: Working with Resources  

E-Print Network (OSTI)

11/30/2006 - 3:00 pm - 4:30 pm Room:San Polo - 3404 (ISD Campus) Autodesk MapGuide® Techniques: Working with Resources The Resource Database and XML Resource documents are a fundamental part of Autodesk Autodesk MapGuide Enterprise application developers how to make the most of these concepts in their own

Ahmad, Sajjad

371

11/30/2006 -5:00 pm -6:30 pm Room:San Polo -3404 (ISD Campus) Autodesk MapGuide Techniques: Sharable Mark-up  

E-Print Network (OSTI)

11/30/2006 - 5:00 pm - 6:30 pm Room:San Polo - 3404 (ISD Campus) Autodesk MapGuide® Techniques industries. This course provides an in-depth look at Autodesk MapGuide Enterprise techniques and APIs-up will be demonstrated while an examination of the code behind the sample will show Autodesk MapGuide Enterprise

Ahmad, Sajjad

372

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)

KU ScholarWorks | http://kuscholarworks.ku.edu Effects of tone on the three-way laryngeal distinction in Korean: An acoustic and aerodynamic comparison of the Seoul and South Kyungsang dialects by Hyunjung Lee and Allard Jongman KU Scholar... below. Lee, H., and Jongman, A. (2012). Effects of tone on the three-way laryngeal distinction in Korean: An acoustic and aerodynamic comparison of the Seoul and South Kyungsang dialects. Journal of the International Phonetic Association 42, 145...

Lee, Hyunjung; Jongman, Allard

2012-08-01T23:59:59.000Z

373

Determination and mapping of diameter and helicity for single-walled carbon nanotubes using nanobeam electron diffraction  

E-Print Network (OSTI)

of the formation energy of carbon nanotubes, while the growth prefers slightly the structure with helicity 15Determination and mapping of diameter and helicity for single-walled carbon nanotubes using June 2005 The atomic structures of 124 single-walled carbon nanotubes, described by their diameter

Qin, Lu-Chang

374

Infrared spectra of individual semiconducting single-walled carbon nanotubes: Testing the scaling of transition energies for large diameter nanotubes  

E-Print Network (OSTI)

of transition energies for large diameter nanotubes Matthew Y. Sfeir and James A. Misewich* Condensed Matter on the same individual nanotube over an energy range of 0.3­2.7 eV. We find that well-established energy scaling relations developed for nanotubes of smaller diameter are not consistent with the measured low-energy

Heinz, Tony F.

375

Laboratory Model of a Contactless Device for Measuring Diameter of Objects with Circular Cross-section Objects  

E-Print Network (OSTI)

and improves the accuracy to measure the outside diameter of optical fibers manufactured at high speed. The device has folow specifications: measuring range: (0.1­1) mm, measuring area 2mm, light sourse ­ laser9 3 Laboratory Model of a Contactless Device for Measuring Diameter of Objects with Circular Cross

Borissova, Daniela

376

The role of apolipoprotein VLDL-II in regulating the diameter of VLDLy  

E-Print Network (OSTI)

OF SUBJECT HENS. . 60 79 VITA 81 LIST OF TABLES TABLE Page 1 Composition of experimental diets . 61 2 Average peak elution times of plasma cholesterol in hens . . . 62 3 Population percentiles for diameter (nm) distributions of VLDL isolated as the d... procedure. 70 Representative standard curves calculated for Apo-VLDL-II and Apo-B in hens fed Diet 1. . 71 Cholesterol elution profiles of d & 1. 0224 g/mL plasma lipoproteins. , 72 Elution times of cholesterol Peak I of d & 1. 0224 g/mL plasma...

Wallowitz, Mikhael L

2012-06-07T23:59:59.000Z

377

Nanotube diameter optimal for channeling of high-energy particle beam  

E-Print Network (OSTI)

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.

V. M. Biryukov; S. Bellucci

2002-06-04T23:59:59.000Z

378

Influence of Diesel Engine Combustion Parameters on Primary Soot Particle Diameter  

Science Journals Connector (OSTI)

In addition to minimized engine-out emissions, exhaust gas after-treatment systems such as diesel particle filter and chemical reduction of NOx will be necessary to meet the U.S. Federal (EPA) 2007 emission standards for heavy-duty diesel engines. ... While for the diesel fuel a reduction of the number of particles in the accumulation mode went in line with a shift of the mode diameter toward smaller values (see Figures 2 and 3), this was not a general observation for the water?diesel emulsion fuel. ... JSME International Journal, Series B: Fluids and Thermal Engineering (2001), 44 (1), 166-170 CODEN: JIJEEE; ISSN:1340-8054. ...

Urs Mathis; Martin Mohr; Ralf Kaegi; Andrea Bertola; Konstantinos Boulouchos

2005-02-04T23:59:59.000Z

379

Library Monday -Thursday Friday Saturday Lied Library 7:30 a.m. -Midnight 7:30 a.m. -7 p.m. 9 a.m. -6 p.m.  

E-Print Network (OSTI)

Library Monday - Thursday Friday Saturday Lied Library 7:30 a.m. - Midnight 7:30 a.m. - 7 p.m. 9 a.m. - 6 p.m. Lied Library - Special Collections 9a.m. -7 p.m. 9 a.m. - 5 p.m. Closed Architecture Studies Library (ASL) 9 a.m. - 9 p.m. 9 a.m. - 5 p.m. Closed Curriculum Materials Library (CML) 8 a.m. - 8 p.m. 8

Hemmers, Oliver

380

Reduction of aerodynamic forces on a minivan by a pair of vortex generators of a pocket type  

Science Journals Connector (OSTI)

Reduction of the aerodynamic forces on a minivan has been achieved using a pair of pockets at the left and the right sides, respectively, of the rear roof end of the vehicle. The two pockets generate cross-streamwise vortices that cause the turbulent kinetic energy to increase in the boundary layer in the downstream of the two pockets. This increased turbulent kinetic energy induces the flow separation to be delayed further downstream along the vehicle back. Unlike the common Vortex Generators (VGs) of extrusive type, these VGs of a pocket type do not cause any additional drag by themselves. This paper investigates numerically the effects of pockets on the reduction of the aerodynamic forces and the flow field around a minivan.

Inchul Kim; Hualei Chen

2010-01-01T23:59:59.000Z

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381

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

SciTech Connect

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

Larry Slone; Jeffrey Birkel

2007-10-31T23:59:59.000Z

382

High Precision Density Measurements of Single Particles: The...  

NLE Websites -- All DOE Office Websites (Extended Search)

to measure individual particle mass spectrometer to measure individual particle aerodynamic diameter and composition. Mobility and aerodynamic diameters are used to extract...

383

Condensed Matter Physics and Materials Science Department (PM)  

NLE Websites -- All DOE Office Websites (Extended Search)

Condensed Matter Physics and Materials Science Department (PM) Condensed Matter Physics and Materials Science Department (PM) Last modified 12/7/2012 LastName First MI Bldg Room Ext1 Ext2 Fax E-mail ABEYKOON MILINDA 510B 1-21 2915 3827 2739 aabeykoon@bnl.gov AKHANJEE SHIMUL 510A 2-6 5089 3995 2918 sakhanjee@bnl.gov ARONSON MEIGAN 703 2A 4915 7090 4071 maronson@bnl.gov BERLIJN TOM COS 3995 3995 tberlijn@bnl.gov BILLINGE SIMON 510B 1-29 5661 3827 2739 sb2896@columbia.edu BLUME MARTIN 510A 1-6 3735 3995 2739 blume@bnl.gov BOLLINGER ANTHONY 480 139 2601 7090 4071 abolling@bnl.gov BOZIN EMIL 510B 1-26 4963 3827 2739 bozin@bnl.gov BOZOVIC IVAN 480 126 4973 7090 4071 bozovic@bnl.gov CHECCO ANTONIO 510B 1-20 3319 3827 2739 checco@bnl.gov CHOU CHUNG-PIN 510A 2-12 3784 3995 2918 cpchou@bnl.gov DAI YAOMIN 510B 1-18 3788 3827 2739 ymdai@bnl.gov DAVIS SEAMUS 480 3827 4071 jcdavis@ccmr.cornell.edu and/or sdavis@bnl.gov DEAN

384

Hangout with Solar Decathlon 2013 Teams on Sept. 18 at 2 pm ET | Department  

Energy.gov (U.S. Department of Energy (DOE)) Indexed Site

Hangout with Solar Decathlon 2013 Teams on Sept. 18 at 2 pm ET Hangout with Solar Decathlon 2013 Teams on Sept. 18 at 2 pm ET Hangout with Solar Decathlon 2013 Teams on Sept. 18 at 2 pm ET September 11, 2013 - 4:24pm Q&A Have questions about the Solar Decathlon? Ask the teams now! Ask Us Addthis Mark your calendars for a Google+ Hangout on Solar Decathlon 2013: The Path to a Brighter Future on Wednesday, Sept. 18, at 2 pm ET. | Photo courtesy of the Energy Department. Mark your calendars for a Google+ Hangout on Solar Decathlon 2013: The Path to a Brighter Future on Wednesday, Sept. 18, at 2 pm ET. | Photo courtesy of the Energy Department. Rebecca Matulka Rebecca Matulka Digital Communications Specialist, Office of Public Affairs How can I participate? Watch it on energy.gov/live or on our Google+ Event page. Tweet questions to @ENERGY with the hashtag #askSD.

385

Effect of lift force on the aerodynamics of dust grains in the protoplanetary disk  

E-Print Network (OSTI)

We newly introduce lift force into the aerodynamics of dust grains in the protoplanetary disk. Although many authors have so far investigated the effects of the drag force, gravitational force and electric force on the dust grains, the lift force has never been considered as a force exerted on the dust grains in the gas disk. If the grains are spinning and moving in the fluid, then the lift force is exerted on them. We show in this paper that the dust grains can be continuously spinning due to the frequent collisions so that the lift force continues to be exerted on them, which is valid in a certain parameter space where the grain size is larger than ~ 1 m and where the distance from the central star is larger than 1 AU for the minimum mass solar nebula. In addition, we estimate the effects of the force on the grain motion and obtain the result that the mean relative velocity between the grains due to the lift force is comparable to the gas velocity in the Kepler rotational frame when the Stokes number and li...

Yamaguchi, Masaki S

2014-01-01T23:59:59.000Z

386

Rather than resonance, flapping wing flyers may play on aerodynamics to improve performance  

E-Print Network (OSTI)

Saving energy and enhancing performance are secular preoccupations shared by both nature and human beings. In animal locomotion, flapping flyers or swimmers rely on the flexibility of their wings or body to passively increase their efficiency using an appropriate cycle of storing and releasing elastic energy. Despite the convergence of many observations pointing out this feature, the underlying mechanisms explaining how the elastic nature of the wings is related to propulsive efficiency remain unclear. Here we use an experiment with a self-propelled simplified insect model allowing to show how wing compliance governs the performance of flapping flyers. Reducing the description of the flapping wing to a forced oscillator model, we pinpoint different nonlinear effects that can account for the observed behavior ---in particular a set of cubic nonlinearities coming from the clamped-free beam equation used to model the wing and a quadratic damping term representing the fluid drag associated to the fast flapping motion. In contrast to what has been repeatedly suggested in the literature, we show that flapping flyers optimize their performance not by especially looking for resonance to achieve larger flapping amplitudes with less effort, but by tuning the temporal evolution of the wing shape (i.e. the phase dynamics in the oscillator model) to optimize the aerodynamics.

Sophie Ramananarivo; Ramiro Godoy-Diana; Benjamin Thiria

2011-08-29T23:59:59.000Z

387

Preliminary Measurements From A New Flat Plate Facility For Aerodynamic Research  

SciTech Connect

This paper details the design and preliminary measurements used in the characterisation of a new flat plate research facility. The facility is designed specifically to aid in the understanding of entropy generation throughout the boundary layer with special attention given to non-equilibrium flows. Hot-wire measurements were obtained downstream of two turbulence generating grids. The turbulence intensity, integral and dissipation length scale ranges measured are 1.6%-7%, 5mm-17mm and 0.7mm-7mm, respectively. These values compared well to existing correlations. The flow downstream of both grids was found to be homogenous and isotropic. Flow visualisation is employed to determine aerodynamic parameters such as flow 2-dimensionality and the effect of the flap angle on preventing separation at the leading edge. The flow was found to be 2-dimensional over all measurement planes. The non-dimensional pressure distribution of a modern turbine blade suction surface is simulated on the flat plate through the use of a variable upper wall. The Reynolds number range based on wetted plate length and inlet velocity is 70,000-4,000,000.

D. M. McEligot; D. W. Nigg; E. J. Walsh; D. Hernon; M.R.D. Davies

2005-03-01T23:59:59.000Z

388

A coupled mesoscale–microscale framework for wind resource estimation and farm aerodynamics  

Science Journals Connector (OSTI)

Abstract This study discusses the development of a coupled mesoscale–microscale framework for wind resource estimation and farm aerodynamics. WINDWYO is a computational framework for performing coupled mesoscale–microscale simulations. The framework is modular, automated and supports coupling of different mesoscale and microscale solvers using overset or matched grids. The modular nature of the framework and the support for overset grids allows the independent development of mesoscale and microscale solvers and the efficient coupling between the codes. The performance of the framework is evaluated by coupling Weather Research and Forecasting (WRF) model with three microscale computational fluid dynamics (CFD) codes of varying complexity. The solvers used are: (i) UWake: a blade element model with free-vortex wake, (ii) Flowyo: large eddy simulation code with actuator line/disk parametrization of the wind turbine and (iii) HELIOS: detached eddy simulation code with full rotor modeling and adaptive mesh refinement. Power predictions and wake visualization of single turbine and off-shore Lillgrund wind farm in uniform and turbulent inflow are used to demonstrate the capabilities of the framework.

Harish Gopalan; Christopher Gundling; Kevin Brown; Beatrice Roget; Jayanarayanan Sitaraman; Jefferey D. Mirocha; Wayne O. Miller

2014-01-01T23:59:59.000Z

389

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

SciTech Connect

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.

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

2012-01-01T23:59:59.000Z

390

Offshore floating vertical axis wind turbines, dynamics modelling state of the art. part I: Aerodynamics  

Science Journals Connector (OSTI)

Abstract The need to further exploit offshore wind resources has pushed offshore wind farms into deeper waters, requiring the use of floating support structures to be economically sustainable. The use of conventional wind turbines may not continue to be the optimal design for floating applications. Therefore it is important to assess other alternative concepts in this context. Vertical axis wind turbines (VAWTs) are one promising concept, and it is important to first understand the coupled and relatively complex dynamics of floating \\{VAWTs\\} to assess their technical feasibility. A comprehensive review detailing the areas of engineering expertise utilised in developing an understanding of the coupled dynamics of floating \\{VAWTs\\} has been developed through a series of articles. This first article details the aerodynamic modelling of VAWTs, providing a review of available models, discussing their applicability to floating \\{VAWTs\\} and current implementations by researchers in this field. A concise comparison between conventional horizontal axis wind turbines and \\{VAWTs\\} is also presented, outlining the advantages and disadvantages of these technologies for the floating wind industry. This article has been written both for researchers new to this research area, outlining underlying theory whilst providing a comprehensive review of the latest work, and for experts in this area, providing a comprehensive list of the relevant references where the details of modelling approaches may be found.

Michael Borg; Andrew Shires; Maurizio Collu

2014-01-01T23:59:59.000Z

391

Sunday, 8th, 2:00 pm Harrison-LeCaine Hall Foyer  

E-Print Network (OSTI)

2013 to May 2014 #12;Friday, 25th, 7:30 pm Dunning Auditorium E-Gré Competition Winner's National TourSunday, 8th, 2:00 pm Harrison-LeCaine Hall Foyer Queen's Conservatory of Music Open House. Check.queensu.ca/qcm Friday, 13th, 12:30 pm Harrison-LeCaine Hall, Rm. 124 Colloquium Presentation by Dr. Kip Pegley, winner

Ellis, Randy

392

Corneal Topography of Excimer Laser Photorefractive Keratectomy Using a 6-mm Beam Diameter  

Science Journals Connector (OSTI)

Objective: The purpose of the study is to define qualitative patterns of corneal topography after excimer laser photorefractive keratectomy (PRK) using a 6-mm beam diameter, investigate changes in patterns over time, and identify associations of topography patterns with clinical outcomes. Design: Multicenter, prospective cohort study. Participants: Ninety-eight eyes of 90 patients with myopia who had undergone PRK using the Summit Technology, Inc., excimer laser with a 6-mm beam diameter. Intervention: Computer-assisted videokeratography data were analyzed for eyes having undergone PRK. Topography patterns at 3, 6, and 12 months after surgery were classified and associations with clinical outcomes assessed. Main Outcomes Measured: Topography patterns after PRK were determined at 3, 6, and 12 months after surgery. Associations with preoperative characteristics of age and attempted correction, and postoperative outcomes of uncorrected and spectacle-corrected visual acuity, predictability, astigmatism, corneal haze, glare, halo, and patient satisfaction were analyzed. Results: At 1 year, 21.4% of corneas showed a homogeneous topography, 27.6% showed a toric-with-axis configuration, 10.2% showed a toric-against-axis configuration, 7.1% showed an irregularly irregular topography, 24.5% showed a keyhole/semicircular pattern, and 9.2% showed focal topographic variants. From 3 to 6 months, 40.1 % of maps changed; from 6 to 12 months, 53.1 % of maps changed, generally to optically smoother, regular patterns. Older age and higher attempted correction were associated with the development of more irregular patterns. The irregular groups showed worse predictability than did the regular groups and a tendency for slight overcorrection. The average reported glare/halo of 1.33 (scale = 0 to 5) in this study was less than in a previous study of the 4.5- to 5-mm treatment zone. However, of six patients expressing dissatisfaction with the results of surgery, three ranked their glare or halo at the maximum level. Conclusions: Topography patterns using a 6-mm beam diameter are identifiable, improve with time, and may affect clinical outcomes after photorefractive keratectomy (PRK). The keyhole/semicircular pattern is more prevalent with a 6 mm treatment zone than with smaller treatment zones. Although optical side effects of glare and halo appear to be reduced with the 6-mm treatment, a small number of patients still report substantial glare or halo after the procedure.

Peter S. Hersh; Shetal I. Shah

1997-01-01T23:59:59.000Z

393

Application of SCR and PM-METALIT for Non-Road Applications: SCRi  

Energy.gov (U.S. Department of Energy (DOE))

Advantages of this new application of SCR and PM-METALIT for non-road applications include compact design, robustness, low backpressure, and cost

394

Evidence for ?_{c}(2S) in ?(3686) \\to ? K_{S}^{0}K^{\\pm}?^{\\mp}?^{+}?^{-}  

E-Print Network (OSTI)

We search for the M1 radiative transition \\psi(3686) \\to \\gamma\\eta_{c}(2S) by reconstructing the exclusive \\eta_{c}(2S) \\to K_{S}^{0}K^{\\pm}\\pi^{\\mp}\\pi^{+}\\pi^{-} decay using 1.06 \\times 10^8 \\psi(3686) events collected with the BESIII detector. The signal is observed with a statistical significance of greater than 4 standard deviations. The measured mass of the \\eta_{c}(2S) is 3646.9 \\pm 1.6(stat) \\pm 3.6(syst) MeV/c^2, and the width is 9.9 \\pm 4.8(stat) \\pm 2.9(syst) MeV/c^2. The product branching fraction is measured to be B(\\psi(3686) \\to \\gamma\\eta_{c}(2S)) \\times B(\\eta_{c}(2S) \\to K_{S}^{0}K^{\\pm}\\pi^{\\mp}\\pi^{+}\\pi^{-}) = (7.03 \\pm 2.10(stat) \\pm 0.70(syst)) \\times 10^{-6}. This measurement complements a previous BESIII measurement of \\psi(3686) \\to \\gamma\\eta_{c}(2S) with \\eta_{c}(2S) \\to K_{S}^{0} K^{\\pm}\\pi^{\\mp} and K^{+}K^{-}\\pi^{0}.

The BESIII Collaboration; M. Ablikim; M. N. Achasov; O. Albayrak; D. J. Ambrose; F. F. An; Q. An; J. Z. Bai; Y. Ban; J. Becker; J. V. Bennett; M. Bertani; J. M. Bian; E. Boger; O. Bondarenko; I. Boyko; R. A. Briere; V. Bytev; X. Cai; O. Cakir; A. Calcaterra; G. F. Cao; S. A. Cetin; J. F. Chang; G. Chelkov; G. Chen; H. S. Chen; J. C. Chen; M. L. Chen; S. J. Chen; X. Chen; Y. B. Chen; H. P. Cheng; Y. P. Chu; D. Cronin-Hennessy; H. L. Dai; J. P. Dai; D. Dedovich; Z. Y. Deng; A. Denig; I. Denysenko; M. Destefanis; W. M. Ding; Y. Ding; L. Y. Dong; M. Y. Dong; S. X. Du; J. Fang; S. S. Fang; L. Fava; F. Feldbauer; C. Q. Feng; R. B. Ferroli; C. D. Fu; J. L. Fu; Y. Gao; C. Geng; K. Goetzen; W. X. Gong; W. Gradl; M. Greco; M. H. Gu; Y. T. Gu; Y. H. Guan; A. Q. Guo; L. B. Guo; Y. P. Guo; Y. L. Han; F. A. Harris; K. L. He; M. He; Z. Y. He; T. Held; Y. K. Heng; Z. L. Hou; H. M. Hu; T. Hu; G. M. Huang; G. S. Huang; J. S. Huang; X. T. Huang; Y. P. Huang; T. Hussain; C. S. Ji; Q. Ji; Q. P. Ji; X. B. Ji; X. L. Ji; L. L. Jiang; X. S. Jiang; J. B. Jiao; Z. Jiao; D. P. Jin; S. Jin; F. F. Jing; N. Kalantar-Nayestanaki; M. Kavatsyuk; W. Kuehn; W. Lai; J. S. Lange; C. H. Li; Cheng Li; Cui Li; D. M. Li; F. Li; G. Li; H. B. Li; J. C. Li; K. Li; Lei Li; Q. J. Li; S. L. Li; W. D. Li; W. G. Li; X. L. Li; X. N. Li; X. Q. Li; X. R. Li; Z. B. Li; H. Liang; Y. F. Liang; Y. T. Liang; G. R. Liao; X. T. Liao; B. J. Liu; C. L. Liu; C. X. Liu; C. Y. Liu; F. H. Liu; Fang Liu; Feng Liu; H. Liu; H. H. Liu; H. M. Liu; H. W. Liu; J. P. Liu; K. Y. Liu; Kai Liu; P. L. Liu; Q. Liu; S. B. Liu; X. Liu; Y. B. Liu; Z. A. Liu; Zhiqiang Liu; Zhiqing Liu; H. Loehner; G. R. Lu; H. J. Lu; J. G. Lu; Q. W. Lu; X. R. Lu; Y. P. Lu; C. L. Luo; M. X. Luo; T. Luo; X. L. Luo; M. Lv; C. L. Ma; F. C. Ma; H. L. Ma; Q. M. Ma; S. Ma; T. Ma; X. Y. Ma; Y. Ma; F. E. Maas; M. Maggiora; Q. A. Malik; Y. J. Mao; Z. P. Mao; J. G. Messchendorp; J. Min; T. J. Min; R. E. Mitchell; X. H. Mo; C. Morales Morales; C. Motzko; N. Yu. Muchnoi; H. Muramatsu; Y. Nefedov; C. Nicholson; I. B. Nikolaev; Z. Ning; S. L. Olsen; Q. Ouyang; S. Pacetti; J. W. Park; M. Pelizaeus; H. P. Peng; K. Peters; J. L. Ping; R. G. Ping; R. Poling; E. Prencipe; M. Qi; S. Qian; C. F. Qiao; X. S. Qin; Y. Qin; Z. H. Qin; J. F. Qiu; K. H. Rashid; G. Rong; X. D. Ruan; A. Sarantsev; B. D. Schaefer; J. Schulze; M. Shao; C. P. Shen; X. Y. Shen; H. Y. Sheng; M. R. Shepherd; X. Y. Song; S. Spataro; B. Spruck; D. H. Sun; G. X. Sun; J. F. Sun; S. S. Sun; Y. J. Sun; Y. Z. Sun; Z. J. Sun; Z. T. Sun; C. J. Tang; X. Tang; I. Tapan; E. H. Thorndike; D. Toth; M. Ullrich; G. S. Varner; B. Wang; B. Q. Wang; D. Wang; D. Y. Wang; K. Wang; L. L. Wang; L. S. Wang; M. Wang; P. Wang; P. L. Wang; Q. Wang; Q. J. Wang; S. G. Wang; X. L. Wang; Y. D. Wang; Y. F. Wang; Y. Q. Wang; Z. Wang; Z. G. Wang; Z. Y. Wang; D. H. Wei; J. B. Wei; P. Weidenkaff; Q. G. Wen; S. P. Wen; M. Werner; U. Wiedner; L. H. Wu; N. Wu; S. X. Wu; W. Wu; Z. Wu; L. G. Xia; Z. J. Xiao; Y. G. Xie; Q. L. Xiu; G. F. Xu; G. M. Xu; H. Xu; Q. J. Xu; X. P. Xu; Z. R. Xu; F. Xue; Z. Xue; L. Yan; W. B. Yan; Y. H. Yan; H. X. Yang; Y. Yang; Y. X. Yang; H. Ye; M. Ye; M. H. Ye; B. X. Yu; C. X. Yu; H. W. Yu; J. S. Yu; S. P. Yu; C. Z. Yuan; Y. Yuan; A. A. Zafar; A. Zallo; Y. Zeng; B. X. Zhang; B. Y. Zhang; C. Zhang; C. C. Zhang; D. H. Zhang; H. H. Zhang; H. Y. Zhang; J. Q. Zhang; J. W. Zhang; J. Y. Zhang; J. Z. Zhang; S. H. Zhang; X. J. Zhang; X. Y. Zhang; Y. Zhang; Y. H. Zhang; Y. S. Zhang; Z. P. Zhang; Z. Y. Zhang; G. Zhao; H. S. Zhao; J. W. Zhao; K. X. Zhao; Lei Zhao; Ling Zhao; M. G. Zhao; Q. Zhao; Q. Z. Zhao; S. J. Zhao; T. C. Zhao; X. H. Zhao; Y. B. Zhao; Z. G. Zhao; A. Zhemchugov; B. Zheng; J. P. Zheng; Y. H. Zheng; B. Zhong; J. Zhong; Z. Zhong; L. Zhou; X. K. Zhou; X. R. Zhou; C. Zhu; K. Zhu; K. J. Zhu; S. H. Zhu; X. L. Zhu; Y. C. Zhu; Y. M. Zhu; Y. S. Zhu; Z. A. Zhu; J. Zhuang; B. S. Zou; J. H. Zou

2013-01-08T23:59:59.000Z

395

Measuring PM Distribution in a Catalyzed Particulate Filter using a Terahertz Wave Scanner  

Energy.gov (U.S. Department of Energy (DOE))

Terahertz scanning system produced 3-dimensional image of local PM density in catatalyzed particulate filters tested under loading and oxidizing conditions

396

Infrared Spectra of Individual Semiconducting Single-walled Carbon Nanotubes: Testing the Scaling of Transition Energies for Large Diameter Nanotubes  

SciTech Connect

We have measured the low-energy excitonic transitions of chiral assigned individual large-diameter semiconducting single-walled nanotubes using a high-resolution Fourier transform photoconductivity technique. When photoconductivity is complemented by Rayleigh scattering spectroscopy, as many as five optical transitions can be identified on the same individual nanotube over an energy range of 0.3-2.7 eV. We find that well-established energy scaling relations developed for nanotubes of smaller diameter are not consistent with the measured low-energy transitions in large (1.8-2.3 nm) diameter nanotubes.

M Sfeir; J Misewich; S Rosenblatt; Y Wu; C Voisin; H Yan; S Berciaud; T Heinz; B Chandra; et al.

2011-12-31T23:59:59.000Z

397

Performance analysis of the cascade impactor, the federal reference method PM 2.5 sampler, and the improve PM 2.5 sampler  

E-Print Network (OSTI)

documented problems with the cascade impactor and suspicions over its accuracy. In this thesis research, the collected PM fractions from the cascade impactor will be subjected to analysis by the Coulter Counter Multisizer to verify inaccuracies. The new FRM...

Buch, Usha-Maria

2012-06-07T23:59:59.000Z

398

Measurements versus Predictions for a Hybrid (Hydrostatic plus Hydrodynamic Thrust Bearing for a Range of Orifice Diameters  

E-Print Network (OSTI)

A fixed geometry hybrid thrust bearing is investigated with three different supply orifice diameters. The test rig uses a face-to-face thrust bearing design, with the test bearing acting as the rotor loading mechanism. A hydraulic shaker applies...

Esser, Paul R.

2011-08-08T23:59:59.000Z

399

Observations of the Origin and Distribution of Ice in Cold, Warm, and Occluded Frontal Systems during the DIAMET Campaign  

Science Journals Connector (OSTI)

Three case studies in frontal clouds from the Diabatic Influences on Mesoscale Structures in Extratropical Storms (DIAMET) project are described to understand the microphysical development of the mixed phase regions of these clouds. The cases are ...

G. Lloyd; C. Dearden; T. W. Choularton; J. Crosier; K. N. Bower

2014-11-01T23:59:59.000Z

400

Impacts of different diameter combinations on the temperature of a crude oil pipeline when colocating with a products pipeline  

Science Journals Connector (OSTI)

In order to show the effects of different diameter combinations on crude oil temperature when a crude oil pipeline and a products pipeline are laid in one trench, four typical ... temperature difference of the cr...

Bo Yu; Yue Shi; Xin Liu; Jinjun Zhang…

2010-06-01T23:59:59.000Z

Note: This page contains sample records for the topic "aerodynamic diameter pm" from the National Library of EnergyBeta (NLEBeta).
While these samples are representative of the content of NLEBeta,
they are not comprehensive nor are they the most current set.
We encourage you to perform a real-time search of NLEBeta
to obtain the most current and comprehensive results.


401

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

E-Print Network (OSTI)

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...

Glenn, Stephen T.

2011-08-08T23:59:59.000Z

402

Multistage axial-flux PM machine for wheel direct drive  

SciTech Connect

The design of direct-drive wheel motors must comply with diameter restriction due to housing the motor in a wheel rim and allow the achievement of very high torque density and overload capability. Slotless axial-flux permanent magnet machines (AFPMs) prove to be the best candidate for application in electric vehicles as direct-drive wheel motors, as in comparison with conventional machines they allow designs with higher compactness, lightness and efficiency. The paper presents a newly conceived AFPM which has a multistage structure and a water-cooled ironless stator. In the proposed new topology of the machine the space formerly occupied by the toroidal core becomes a water duct, which removes heat directly from the interior surface of the stator winding. The high efficiency of the machine cooling arrangement allows long-term 100% overload operation and great reduction of the machine weight. The multistage structure of the machine is suited to overcome the restriction on the machine diameter and meet the torque required at the wheel shaft. The paper gives guidelines for the design of a multistage AFPM with water-cooled ironless stator, and describes characteristics of a two-stage prototype machine rated 215 N{center_dot}m, 1,100 r/min.

Caricchi, F.; Crescimbini, F.; Mezzetti, F.; Santini, E. [Univ. of Rome La Sapienza (Italy). Dept. of Electrical Engineering] [Univ. of Rome La Sapienza (Italy). Dept. of Electrical Engineering

1996-07-01T23:59:59.000Z

403

Mitigating wind-turbine induced avian mortality: Sensory, aerodynamic and cognitive constraints and options  

Science Journals Connector (OSTI)

Abstract Because of the fast rate of wind-energy development it will become a challenge to verify impacts on birdlife and construe ways to minimise these. Birds colliding with wind turbines are generally perceived as one of the major conflict issues for wind-energy development. Development of effective and practical measures to reduce bird mortality related to offshore and onshore wind energy is therefore paramount to avoid any delay in consenting processes. The expected efficacy of post-construction mitigation measures for wind-turbine induced avian mortality can be expected to be species-specific with regard to audible, optical and biomechanical constraints and options. Species-specific sensory faculties limit the ability to observe a wind turbine in a given circumstance. Their consequent cognitive perception may depend on the possibilities for associating wind turbines with risk, and discriminating these from other sources. Last but not least, perceived risks may only be evaded when their aerodynamic, locomotive physiology enables them to do so in due time. In order to be able to identify and construe functional mitigation measures these aspects need to be taken into account. Measures eliciting a series of intermittent strong stimuli that are variable in frequency may limit habituation effects; these should only be elicited specifically to mitigate imminent collision. Thus measures either adjusting turbine operation or warning/deterring birds approaching turbines are expected to be most functional. Warning signals may either be based on optical or audible stimuli; however, birds? hearing is inferior to humans while their visual acuity and temporal resolution is higher, but with great differences among species. Implementing effective mitigation measures could reduce the general level of conflicts with birdlife and thus enable both the development at new sites, at sites that have been declared having too high conflict levels, and utilise the wind resources better at specific sites without increasing the conflict levels.

R. May; O. Reitan; K. Bevanger; S.-H. Lorentsen; T. Nygård

2015-01-01T23:59:59.000Z

404

Biomedical Engineering -Student Composite June 26, 2014, 6:00 pm Anas Abidin  

E-Print Network (OSTI)

Biomedical Engineering - Student Composite June 26, 2014, 6:00 pm Anas Abidin Wism�¼ller Lab Seth Lab Christopher Farrar First Year Gary Fino First Year Page 1/4 #12;Biomedical Engineering - Student Benjamin Miller Lab Page 2/4 #12;Biomedical Engineering - Student Composite June 26, 2014, 6:00 pm Alvin

Goldman, Steven A.

405

A Systemic Design Methodology of PM Generators for Fixed-Pitch Marine Current Turbines  

E-Print Network (OSTI)

A Systemic Design Methodology of PM Generators for Fixed-Pitch Marine Current Turbines Sofiane of permanent magnet (PM) generator associated with fixed-pitch turbine for tidal energy generation. The main problem with marine current turbines systems are the maintenance requirements of the drive

Paris-Sud XI, Université de

406

DSM-PM2: A portable implementation platform for multithreaded DSM consistency protocols  

E-Print Network (OSTI)

DSM-PM2: A portable implementation platform for multithreaded DSM consistency protocols Gabriel Antoniu and Luc Bougé Abstract DSM-PM2 is a platform for designing, implementing and experimenting multithreaded DSM consistency proto- cols. It provides a generic toolbox which facilitates protocol design

Paris-Sud XI, Université de

407

UNCORRECTEDPROOF SPB-190570 Chapter ID 19 August 4, 2010 Time: 01:07pm Proof 1  

E-Print Network (OSTI)

UNCORRECTEDPROOF SPB-190570 Chapter ID 19 August 4, 2010 Time: 01:07pm Proof 1 01 02 03 04 05 06 07, LLC 2011 #12;UNCORRECTEDPROOF SPB-190570 Chapter ID 19 August 4, 2010 Time: 01:07pm Proof 1 46 47 48. Most studies supporting the DOHaD hypoth- esis are primarily nutritional in nature, thus the potential

Blumberg, Bruce

408

American Conference on Neutron Scattering M4-C4 (5:15 pm)  

E-Print Network (OSTI)

50 American Conference on Neutron Scattering M4-C4 (5:15 pm) aCORN: A New MeasurementBeamlineatSnS.Inthistalk,theprinciple oftheexperiment,andthestatusofongoingR&d willbereviewedanddiscussed. M4-C6 (5:45 pm) Neutron-proton Scattering of the Electron- antineutrino Correlation Coefficient in Neutron Decay M. Leuschner (Indiana University Cyclotron

Danon, Yaron

409

SEALING LARGE-DIAMETER CAST-IRON PIPE JOINTS UNDER LIVE CONDITIONS  

SciTech Connect

Utilities in the U.S. operate over 75,000 km (47,000 miles) of old cast-iron pipes for gas distribution. The 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 cast-iron bell and spigot joints from a single pipe entry point. The proposed system will perform repairs while the pipe remains 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, 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 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 repair operations on live mains. The development effort is divided into eleven tasks. Task 1--Program Management and Task 2--were completed in prior quarters while Task 3--Design and Fabricate Ratcheting Stainless-Steel Repair Sleeves has progressed to installing prototype sleeves in cast iron test pipe segments. Efforts in this quarter continued to focus on Tasks 4--8, with significant progress made in each. Task 4 (Design, Fabricate and Test Patch Setting Robotic Train) progressed to the design of the control electronics and pneumatic system to inflate the bladder robotic patch setting module. Task 5 (Design & Fabricate Pipe-Wall Cleaning Robot Train with Pan/Zoom/Tilt Camera) continued with additional in-pipe testing required to optimize the design of the robot elements and surface control electronics and software. Task 6 (Design & Build Surface Control and Monitoring System) has been completed with the control and computer display functions being operated through LabView. Task 7 (Design & Fabricate Large Diameter Live Access System) progressed to completing the detailed design of the entry fitting for 12-inch diameter cast iron pipe. The fitting is now being placed into manufacture. Task 8--System Integration and Laboratory Validation continued developing the robot module inter-connects and development of a master LabView-based system display and control software.

Kiran M. Kothari; Gerard T. Pittard

2004-04-01T23:59:59.000Z

410

SEALING LARGE-DIAMETER CAST-IRON PIPE JOINTS UNDER LIVE CONDITIONS  

SciTech Connect

Utilities in the U.S. operate over 75,000 km (47,000 miles) of old cast-iron pipes for gas distribution. The 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 while the pipe remains 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, 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 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 repair operations on live mains. The development effort is divided into eleven tasks. Task 1 (Program Management) and Task 2 (Establishment of Detailed Design Specifications) were completed in prior quarters while Task 3 (Design and Fabricate Ratcheting Stainless-Steel Repair Sleeves) has progressed to installing prototype sleeves in cast iron test pipe segments. Efforts in this quarter continued to focus on Tasks 4-8, with significant progress made in each. Task 4 (Design, Fabricate and Test Patch Setting Robotic Train) progressed to the design of the control electronics and pneumatic system to inflate the bladder robotic patch setting module. Task 5 (Design & Fabricate Pipe-Wall Cleaning Robot Train with Pan/Zoom/Tilt Camera) continued with additional in-pipe testing required to optimize the design of the robot elements and surface control electronics and software. Task 6 (Design & Build Surface Control and Monitoring System) has been completed with the control and computer display functions being operated through LabView. Task 7 (Design & Fabricate Large Diameter Live Access System) progressed to completing the detailed design of the entry fitting for 12-inch diameter cast iron pipe. The fitting is now being manufactured. The 12-inch ball valve for allowing no-blow access was also procured. Task 8 (System Integration and Laboratory Validation) continued with the development of the robot module inter-connects and of a master LabView-based system display and control software.

Kiran M Kothari; Gerard T. Pittard

2004-07-01T23:59:59.000Z

411

SEALING LARGE-DIAMETER CAST-IRON PIPE JOINTS UNDER LIVE CONDITIONS  

SciTech Connect

Utilities in the U.S. operate over 75,000 km (47,000 miles) of old cast-iron pipes for gas distribution. The 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 cast iron bell and spigot joints from a single pipe entry point. The proposed system will perform repairs while the pipe remains 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, 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 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 repair operations on live mains. The development effort is divided into eleven tasks. Task 1--Program Management and Task 2--were completed in prior quarters while Task 3--Design and Fabricate Ratcheting Stainless-Steel Repair Sleeves has progressed to installing prototype sleeves in cast iron test pipe segments. Efforts in this quarter continued to focus on Tasks 4--8, with significant progress made in each. Task 4 (Design, Fabricate and Test Patch Setting Robotic Train) progressed to the design of the control electronics and pneumatic system to inflate the bladder robotic patch setting module. Task 5 (Design & Fabricate Pipe-Wall Cleaning Robot Train with Pan/Zoom/Tilt Camera) continued with additional in-pipe testing required to optimize the design of the robot elements and surface control electronics and software. Task 6 (Design & Build Surface Control and Monitoring System) has been completed with the control and computer display functions being operated through LabView. Task 7 (Design & Fabricate Large Diameter Live Access System) progressed to the design, fabrication and testing of a entry fitting in a 4-inch prototype and is now being used to complete drawings for use in 12-inch diameter pipe. Task 8--System Integration and Laboratory Validation continued developing the robot module inter-connects and development of a master LabView-based system display and control software.

Kiran M. Kothari, Gerard T. Pittard

2004-01-01T23:59:59.000Z

412

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

SciTech Connect

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

McCallen, R

2002-09-01T23:59:59.000Z

413

Today at 2:30 pm ET: Hangout With Science, Tech, and Innovation Leaders |  

Energy.gov (U.S. Department of Energy (DOE)) Indexed Site

Today at 2:30 pm ET: Hangout With Science, Tech, and Innovation Today at 2:30 pm ET: Hangout With Science, Tech, and Innovation Leaders Today at 2:30 pm ET: Hangout With Science, Tech, and Innovation Leaders February 27, 2013 - 9:00am Q&A What questions do you have about science, tech, engineering and math (STEM) education and careers? Ask Us Addthis Join our Google+ Hangout on bridging the diversity gap in STEM education and careers at 2:30 pm ET today. | Graphic courtesy of Sarah Gerrity. Join our Google+ Hangout on bridging the diversity gap in STEM education and careers at 2:30 pm ET today. | Graphic courtesy of Sarah Gerrity. Dot Harris Dot Harris The Honorable Dot Harris, Director, Office of Economic Impact and Diversity

414

COLLOQUIUM - NOTE SPECIAL TIME OF 3:15PM: Savannah River National  

NLE Websites -- All DOE Office Websites (Extended Search)

May 15, 2013, 3:15pm to 5:30pm May 15, 2013, 3:15pm to 5:30pm Colloquia MBG Auditorium COLLOQUIUM - NOTE SPECIAL TIME OF 3:15PM: Savannah River National Laboratory: Underpinning Critical National Missions Dr. Jeff Griffin Savannah River National Laboratory The Cold War mission of the Savannah River Site in South Carolina was to produce nuclear materials for the national defense. Since the Cold War ended, SRS has continued to ensure United States national and energy security while cleaning up the environmental legacy from nuclear materials production. Throughout the history of SRS, the Savannah River National Laboratory has developed the processes to successfully accomplish the site's missions. SRNL is a multi-program laboratory dedicated to addressing the nation's present and future challenges in National Security, Clean Energy, and

415

The orifice expansion correction for a 50 mm line size at various diameter ratios  

SciTech Connect

The expansion coefficient or factor for a compressible flowmeter corrects for the change in pressure and density as the fluid is accelerated through the flowmeter. The expansion correction currently in use in the United States and also in other countries was developed over fifty years ago by Buckingham and Bean. More recent work reported by Kinghorn shows the equation currently in use to be in error. This paper describes the results of a test program to determine the expansion factors for flange-tapped sharp-edged orifices with diameter ratios between 0.242 and 0.726 in a nominal 50 mm (2 inch) line. Critical flow Venturis are used as the reference standards and dry air as the flowing fluid. The ratio of differential pressure to inlet static pressure is varied over a range of zero to about 0.2 at a constant Reynolds number. The expansion factor is determined form the apparent change in discharge coefficient at a constant Reynolds number.

Seidl, W. [Colorado Engineering Experiment Station, Inc., Nunn, CO (United States)

1995-12-31T23:59:59.000Z

416

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

DOE Patents (OSTI)

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.

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

2002-01-29T23:59:59.000Z

417

An 8-mm diameter Fiber Robot Positioner for Massive Spectroscopy Surveys  

E-Print Network (OSTI)

Massive spectroscopic survey are becoming trendy in astrophysics and cosmology, as they can address new fundamental knowledge such as Galactic Archaeology and probe the nature of the mysterious Dark Energy. To enable massive spectroscopic surveys, new technology are being developed to place thousands of optical fibers at a given position on a focal plane. These technology needs to be: 1) accurate, with micrometer positional accuracy; 2) fast to minimize overhead; 3) robust to minimize failure; and 4) low cost. In this paper we present the development of a new 8-mm in diameter fiber positionner robot using two 4mm DC-brushless gearmotors, developed in the context of the Dark Energy Spectroscopic Instrument. This development was conducted by a Spanish-Swiss (ES-CH) team led by the Instituto de F\\'isica Te\\'orica (UAM-CSIC) and the Laboratoire d'Astrophysique (EPFL), in collaboration with the AVS company in Spain and the Faulhaber group (MPS & FAULHABER-MINIMOTOR) in Switzerland.

Fahim, Nasib; Kneib, Jean Paul

2014-01-01T23:59:59.000Z

418

SEALING LARGE-DIAMETER CAST-IRON PIPE JOINTS UNDER LIVE CONDITIONS  

SciTech Connect

Utilities in the U.S. operate over 75,000 km (47,000 miles) of old cast-iron pipes for gas distribution. The 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 cast-iron bell and spigot joints from a single pipe entry point. The proposed system will perform repairs while the pipe remains 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, 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 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 repair operations on live mains. The development effort is divided into eleven tasks. Task 1 (Program Management) and Task 2 (Establishment of Detailed Design Specifications) were completed in prior quarters while Task 3 (Design and Fabricate Ratcheting Stainless-Steel Repair Sleeves) has progressed to installing prototype sleeves in cast-iron test pipe segments. Efforts in the current quarter continued to focus on Tasks 4-8. Highly valuable lessons were learned from field tests of the 4-inch gas pipe repair robot in cast-iron pipe at Public Service Electric & Gas. (These field tests were conducted and reported last quarter.) These tests identified several design issues which need to be implemented in both the small- and large-diameter repair robots for cast-iron pipe to assure their commercial success. For Task 4 (Design, Fabricate and Test Patch Setting Robotic Train), work has been directed on increasing the nitrogen bladder reservoir volume to allow at least two complete patch inflation/patch setting cycles in the event the sleeve does not set all ratchets in the same row on the first attempt. This problem was observed on a few of the repair sleeves that were recently installed during field tests with the small-diameter robotic system. For Task 5 (Design & Fabricate Pipe-Wall Cleaning Robot Train with Pan/Zoom/Tilt Camera), the recent field tests showed clearly that, in mains with low gas velocities, it will be necessary to improve the system's capacity to remove debris from the immediate vicinity of the bell and spigot joints. Otherwise, material removed by the cleaning flails (the flails were found to be very effective in cleaning bell and spigot joints) falls directly to the low side of the pipe and accumulates in a pile. This accumulation can prevent the sleeve from achieving a leak-free repair. Similarly, it is also deemed necessary to design an assembly to capture existing service-tap coupons and allow their removal from the inside of the pipe. These coupons were found to cause difficulty in launching and retrieving the small pipe repair robot; for example, one coupon lodged beneath the end of the guide shoe. Designs for new features to accomplish these goals for the large robotic system were pursued and are presented in this report. Task 6 (Design & Build Surface Control and Monitoring System) was previously completed with the control and computer display functions being operated through LabVIEW. However, this must now be revisited to add control routines for the coupon catcher to be added. This will most likely include a lift-off/place-on magnet translation function. Task 7 (Design & Fabricate Large Diameter Live Access System) progressed to completing the detailed design of the entry fitting for 12-inch diameter cast iron pipe in the previous quarter. Field tests with the 4-inch

Kiran M. Kothari; Gerard T. Pittard

2005-01-01T23:59:59.000Z

419

Case study of landfill leachate recirculation using small-diameter vertical wells  

Science Journals Connector (OSTI)

Abstract A case study of landfill liquids addition using small diameter (5 cm) vertical wells is reported. More than 25,000 m3 of leachate was added via 134 vertical wells installed 3 m, 12 m, and 18 m deep over five years in a landfill in Florida, US. Liquids addition performance (flow rate per unit screen length per unit liquid head) ranged from 5.6 × 10?8 to 3.6 × 10?6 m3 s?1 per m screen length per m liquid head. The estimated radial hydraulic conductivity ranged from 3.5 × 10?6 to 4.2 × 10?4 m s?1. The extent of lateral moisture movement ranged from 8 to 10 m based on the responses of moisture sensors installed around vertical well clusters, and surface seeps were found to limit the achievable liquids addition rates, despite the use of concrete collars under a pressurized liquids addition scenario. The average moisture content before (51 samples) and after (272 samples) the recirculation experiments were 23% (wet weight basis) and 45% (wet weight basis), respectively, and biochemical methane potential measurements of excavated waste indicated significant (p < 0.025) decomposition.

Pradeep Jain; Jae Hac Ko; Dinesh Kumar; Jon Powell; Hwidong Kim; Lizmarie Maldonado; Timothy Townsend; Debra R. Reinhart

2014-01-01T23:59:59.000Z

420

SEALING LARGE-DIAMETER CAST-IRON PIPE JOINTS UNDER LIVE CONDITIONS  

SciTech Connect

Utilities in the U.S. operate over 75,000 km (47,000 miles) of old cast-iron pipes for gas distribution. The 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 while the pipe remains 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, 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 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 repair operations on live mains. The development effort is divided into eleven tasks. Task 1 (Program Management) and Task 2 (Establishment of Detailed Design Specifications) were completed in prior quarters while Task 3 (Design and Fabricate Ratcheting Stainless-Steel Repair Sleeves) has progressed to installing prototype sleeves in cast iron test pipe segments. Efforts in this quarter continued to focus on Tasks 4-8, with significant progress made in each as well as field testing of the 4-inch gas pipe repair robot in cast iron pipe at Public Service Electric & Gas. The field tests were conducted August 23-26, 2004 in Oradell, New Jersey. The field tests identified several design issues which need to be implemented in both the small- and large-diameter cast iron repair robots to assure their commercial success. Task 4 (Design, Fabricate and Test Patch Setting Robotic Train) progressed to the design of the control electronics and pneumatic system to inflate the bladder robotic patch setting module in the last quarter 5. In this quarter, work has been concentrated on increasing the nitrogen bladder reservoir volume to allow at least two complete patch inflation/patch setting cycles in the event the sleeve does not set all ratchets in the same row on the first attempt. This problem was observed on a few of the repair sleeves that were recently installed during field tests with the small-diameter robotic system. For Task 5 (Design & Fabricate Pipe-Wall Cleaning Robot Train with Pan/Zoom/Tilt Camera) it was observed that it will be necessary to add a stiff brush to push debris away from the immediate vicinity of the bell and spigot joints in mains having low gas velocities. Otherwise, material removed by the cleaning flails (which were found to be very effective in cleaning bell and spigot joints) simply falls to the low side of the pipe and accumulates in a pile. This accumulation can prevent the sleeve from achieving a leak free repair. Similarly, it is also necessary to design a small magnet to capture existing service tap coupons and allow their removal from the inside of the pipe. These coupons were found to cause difficulty in launching and retrieving the small pipe repair robot; one coupon lodged beneath the end of the guide shoe. These new features require redesign of the pipe wall cleaning train and modification to the patch setting train. Task 6 (Design & Build Surface Control and Monitoring System) was previously completed with the control and computer display functions being operated through LabView. However, this must now be re-visited to add control routines for the coupon catcher to be added. This will most likely include a lift-off/place-on magnet translation function. Task 7 (Design & Fabricate Large Diameter Live Access System) progressed to completing the detailed design of th

Kiran M. Kothari; Gerard T. Pittard

2004-11-01T23:59:59.000Z

Note: This page contains sample records for the topic "aerodynamic diameter pm" from the National Library of EnergyBeta (NLEBeta).
While these samples are representative of the content of NLEBeta,
they are not comprehensive nor are they the most current set.
We encourage you to perform a real-time search of NLEBeta
to obtain the most current and comprehensive results.


421

SEALING LARGE-DIAMETER CAST-IRON PIPE JOINTS UNDER LIVE CONDITIONS  

SciTech Connect

Utilities in the U.S. operate over 75,000 km (47,000 miles) of old cast-iron pipes for gas distribution. The 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 cast-iron bell and spigot joints from a single pipe entry point. The proposed system will perform repairs while the pipe remains 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, 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 repair operations on live mains. The development effort is divided into eleven tasks. Task 1 (Program Management) and Task 2 (Establishment of Detailed Design Specifications) were completed previously. Task 3 (Design and Fabricate Ratcheting Stainless-Steel Repair Sleeves) has progressed to installing prototype sleeves in test cast-iron pipe segments. Efforts in the current quarter continued to be focused on Tasks 4-8. Highly valuable lessons were learned from field tests of the 4-inch gas pipe repair robot in cast-iron pipe at Public Service Electric & Gas. (These field tests were conducted and reported previously.) Several design issues were identified which need to be implemented in both the small- and large-diameter repair robots for cast-iron pipe to assure their commercial success. For Task 4 (Design, Fabricate and Test Patch Setting Robotic Train), previous problems with bladder design and elastomeric material expansion in the large mains were addressed. A new bladder based on a commercially available design was obtained and tested with success. Minor improvements were highlighted during patch-setting tests and are now being pursued. For Task 5 (Design and Fabricate Pipe-Wall Cleaning Robot Train with Pan/Zoom/Tilt Camera), the previous field tests showed clearly that, in mains with low gas velocities, it will be necessary to improve the system's capacity to remove debris from the immediate vicinity of the bell and spigot joints. Otherwise, material removed by the cleaning flails (the flails were found to be very effective in cleaning bell and spigot joints) falls directly to the low side of the pipe and accumulates in a pile. This accumulation can prevent the sleeve from achieving a leak-free repair. Similarly, it is also deemed necessary to design an assembly to capture existing servicetap coupons and allow their removal from the inside of the pipe. Task 6 (Design and Build Surface Control and Monitoring System) was previously completed with the control and computer display functions being operated through LabVIEW. However, this must now be revisited to add control routines for the coupon catcher that will be added. This will most likely include a lift-off/place-on magnet translation function. Task 7 (Design and Fabricate Large Diameter Live Access System) progressed to completing the detailed design for a bolt-on entry fitting for 12-inch diameter cast-iron pipe in the current quarter. The drilling assembly for cutting an access hole through the wall of the gas main was also designed, along with a plug assembly to allow removing all tools from the live main and setting a blind flange on the entry fitting prior to burial. These designs are described in detail in the report. Task 8 (System Integration and Laboratory Validation) continued with the development of the robot module i

Kiran M. Kothari; Gerard T. Pittard

2005-04-01T23:59:59.000Z

422

NETL: Ambient Monitoring - Characterization of Ambient PM2.5 in the Upper  

NLE Websites -- All DOE Office Websites (Extended Search)

Characterization of Ambient PM2.5 in the Upper Midwest Characterization of Ambient PM2.5 in the Upper Midwest As part of a Cooperative Agreement with DOE-NETL, the University of North Dakota Energy and Environmental Research Center (EERC) is developing advanced sampling and analysis methodologies for particulate matter that can be used for source apportionment and to assist in health studies. These techniques will be used to determine sources of fine particulate matter in rural states such as North Dakota. Ambient particulate matter (PM) sampling and automated scanning electron microscopy, (ASEM) are being used to characterize and evaluate the sources of PM2.5 at three rural sites. Land use in the sampling site locations is dominated by ranching and small grain farming. Potential sources of PM in these areas include diesel- and gasoline-fueled motor vehicles, fugitive dust from gravel roads and agriculture, vegetation and fires, an oil refinery, and coal-fired power plants. PM2.5 samples were collected using an automatic cartridge collection unit for ASEM analysis. An ASEM method has been developed to size and chemically classify individual particles composing PM2.5.

423

Interested in STEM? Join us for a Tweet-up This Thursday at 4pm ET |  

Energy.gov (U.S. Department of Energy (DOE)) Indexed Site

Interested in STEM? Join us for a Tweet-up This Thursday at 4pm ET Interested in STEM? Join us for a Tweet-up This Thursday at 4pm ET Interested in STEM? Join us for a Tweet-up This Thursday at 4pm ET May 8, 2012 - 3:37pm Q&A What do you want to know about the Energy Department's work in STEM investment? Ask Us Addthis Join Michelle Fox on Twitter this Thursday at 4:00pm for a Tweet-up about STEM investments in education and the workforce. Join Michelle Fox on Twitter this Thursday at 4:00pm for a Tweet-up about STEM investments in education and the workforce. Amanda Scott Amanda Scott Former Managing Editor, Energy.gov How can I participate? Send us your questions via Twitter (@ENERGY) using #STEM. Email us your questions at newmedia@hq.doe.gov. Join us on Thursday, May 10 at 4:00pm ET to get your questions answered on Twitter (@ENERGY).

424

Indoor-Outdoor Concentrations and Correlations of PM10-Associated Mutagenic Activity in Nonsmokers' and Asthmatics' Homes  

Science Journals Connector (OSTI)

Indoor-Outdoor Concentrations and Correlations of PM10-Associated Mutagenic Activity in Nonsmokers' and Asthmatics' Homes ...

Norman Y. Kado; Steven D. Colome; Michael T. Kleinman; Dennis P. H. Hsieh; Peter. Jaques

1994-06-01T23:59:59.000Z

425

Estimation of exhaust gas aerodynamic force on the variable geometry turbocharger actuator: 1D flow model approach  

Science Journals Connector (OSTI)

Abstract This paper provides a reliable tool for simulating the effects of exhaust gas flow through the variable turbine geometry section of a variable geometry turbocharger (VGT), on flow control mechanism. The main objective is to estimate the resistive aerodynamic force exerted by the flow upon the variable geometry vanes and the controlling actuator, in order to improve the control of vane angles. To achieve this, a 1D model of the exhaust flow is developed using Navier–Stokes equations. As the flow characteristics depend upon the volute geometry, impeller blade force and the existing viscous friction, the related source terms (losses) are also included in the model. In order to guarantee stability, an implicit numerical solver has been developed for the resolution of the Navier–Stokes problem. The resulting simulation tool has been validated through comparison with experimentally obtained values of turbine inlet pressure and the aerodynamic force as measured at the actuator shaft. The simulator shows good compliance with experimental results.

Fayez Shakil Ahmed; Salah Laghrouche; Adeel Mehmood; Mohammed El Bagdouri

2014-01-01T23:59:59.000Z

426

Sun. Sept. 15th LILY G458 7:30-9PM Sun. Oct. 13th LILY G458 7:30 ...  

E-Print Network (OSTI)

Sun. Sept. 15th LILY G458 7:30-9PM. Sun. Oct. 13th LILY G458 7:30-9PM. Mon. Nov. 11th BRNG 1232 7:30-9PM. For more information please. Contact:.

LYNETTE

2013-08-16T23:59:59.000Z

427

On the influence that the ground electrode diameter has in the propulsion efficiency of an asymmetric capacitor in nitrogen gas  

SciTech Connect

In this work, the propulsion force developed in an asymmetric capacitor will be calculated for three different diameters of the ground electrode. The used ion source is a small diameter wire, which generates a positive corona discharge in nitrogen gas directed to the ground electrode. By applying the fluid dynamic and electrostatic theories, all hydrodynamic and electrostatic forces that act on the considered geometries will be computed in an attempt to provide a physical insight on the force mechanism that acts on the asymmetrical capacitors, and also to understand how to increase the efficiency of propulsion.

Martins, Alexandre A. [Institute for Plasmas and Nuclear Fusion, Instituto Superior Tecnico, Av. Rovisco Pais, 1049-001 Lisboa (Portugal); Pinheiro, Mario J. [Department of Physics and Institute for Plasmas and Nuclear Fusion, Instituto Superior Tecnico, Av. Rovisco Pais, 1049-001 Lisboa (Portugal)

2011-03-15T23:59:59.000Z

428

B2223 High Temperature Superconductor Wires in Silver Sheath, Filament Diameter Effect on Critical Temperature and Current Density  

Science Journals Connector (OSTI)

B2223 High Temperature Superconductor (HTSC) has been prepared as a pellet by solid state reaction. Then, HTSC wires were fabricated from the prepared superconductor using powder in tube (PIT) method utilizing silver as the tube material. Superconductor powder was packed in the pure silver tube of about 4.5 mm diameter, and 50 mm long. The prepared wires are of three types; with monofilament MOF, 9 multifilament core (9MF) and 81 filaments core(81MF). Several cycles of mechanical are drawing and rolling process performed to the starting silver tube of 0.4 cm diameter and 5 cm length and 0.35 mm thickness to minimize the filament diameter. The average filament diameter of MoC with 0.7 mm SC core which was produce by the first step of drawing, the second 9 MF wire with nine multifilament wire of 0.175 mm diameter for each filament,while the 81MFC wire filament diameter was about 25 ?m for each filament measured with an optical microscope. All the three types of wires were with same outer diameter of 0.9 mm. Tc critical temperature for superconductivity is measured for the pellet and wires using four point probes techniques. The critical temperature for the pellet is 110 °K, for the monofilament MOF is 112.5 °K and for 9 filaments 9MF was found is 117°K; while the Tc the 81MF was 119.5°K. The critical current density for the 9MF and 81MF wires were found higher than that of the monofilament MOF in spite of the smaller filament diameters of the 9 MF and 81MF. X-ray diffraction pattern shows the high Tc phase of B2223 compounds in addition to low phase, of B2212 compounds. The I-V curves for the three different wires show higher current density for 81 MF wire, while the optical microscope picture shows more grains alignment . MOC and 9 MF wires show misalignment grains.

Akram R. Jabur

2012-01-01T23:59:59.000Z

429

4:45PM ET TODAY: On-the-Record Conference Call with Administration, Jobs  

Energy.gov (U.S. Department of Energy (DOE)) Indexed Site

4:45PM ET TODAY: On-the-Record Conference Call with Administration, 4:45PM ET TODAY: On-the-Record Conference Call with Administration, Jobs Council Officials to Discuss the Obama Administration's Announcement of 14 Initial Partners in the Better Buildings Challenge 4:45PM ET TODAY: On-the-Record Conference Call with Administration, Jobs Council Officials to Discuss the Obama Administration's Announcement of 14 Initial Partners in the Better Buildings Challenge June 30, 2011 - 12:00am Addthis THE WHITE HOUSE Office of the Press Secretary WASHINGTON, D.C. - Today at 4:45PM ET, Senior Administration Officials Maria Vargas and Michelle Moore, and Member of the President's Jobs Council Laura Tyson will hold an on-the-record conference call to discuss the Administration's announcement today at the Clinton Global Initiative America meeting of 14 initial partners in the Better Buildings Challenge.

430

Definition: Reduced Sox, Nox, And Pm-2.5 Emissions | Open Energy  

Open Energy Info (EERE)

Sox, Nox, And Pm-2.5 Emissions Sox, Nox, And Pm-2.5 Emissions Jump to: navigation, search Dictionary.png Reduced Sox, Nox, And Pm-2.5 Emissions Functions that provide this benefit can lead to avoided vehicle miles, decrease the amount of central generation needed to their serve load (through reduced electricity consumption, reduced electricity losses, more optimal generation dispatch), and or reduce peak generation. These impacts translate into a reduction in pollutant emissions produced by fossil-based electricity generators and vehicles.[1] Related Terms electricity generation, reduced electricity losses, smart grid References ↑ SmartGrid.gov 'Description of Benefits' An in LikeLike UnlikeLike You like this.Sign Up to see what your friends like. line Glossary Definition Retrieved from "http://en.openei.org/w/index.php?title=Definition:Reduced_Sox,_Nox,_And_Pm-2.5_Emissions&oldid=502508

431

Hangout with Clean Cities on Thursday, June 20, at 2:30 pm ET | Department  

Energy.gov (U.S. Department of Energy (DOE)) Indexed Site

Hangout with Clean Cities on Thursday, June 20, at 2:30 pm ET Hangout with Clean Cities on Thursday, June 20, at 2:30 pm ET Hangout with Clean Cities on Thursday, June 20, at 2:30 pm ET June 13, 2013 - 5:45pm Q&A Want to know what we are doing to cut the nation's oil use in transportation? Ask Us Addthis Mark your calendars for a Google+ Hangout on Clean Cities: Celebrating 20 Years of Sustainable Transportation. | Photo courtesy of the Energy Department. Mark your calendars for a Google+ Hangout on Clean Cities: Celebrating 20 Years of Sustainable Transportation. | Photo courtesy of the Energy Department. Rebecca Matulka Rebecca Matulka Digital Communications Specialist, Office of Public Affairs How can I participate? Sign up at the Google+ Event page. Tweet questions to @ENERGY with the hashtag #AskEnergy. Ask us on the Energy Department's Facebook and Google+ pages.

432

#LabChat: Extreme Circumstances, Unique Solutions, June 28 at 1pm EDT |  

Energy.gov (U.S. Department of Energy (DOE)) Indexed Site

Extreme Circumstances, Unique Solutions, June 28 at 1pm Extreme Circumstances, Unique Solutions, June 28 at 1pm EDT #LabChat: Extreme Circumstances, Unique Solutions, June 28 at 1pm EDT June 27, 2012 - 2:31pm Addthis The simple, portable device identifies materials through their characteristic energy signals as unique as fingerprints. The three detectors are housed in a thermos-sized container that is connected to a laptop computer. The device issues a signal turning the laptop display bright red when nuclear material of interest is identified. | Photo courtesy of Princeton University The simple, portable device identifies materials through their characteristic energy signals as unique as fingerprints. The three detectors are housed in a thermos-sized container that is connected to a laptop computer. The device issues a signal turning the laptop display

433

LiveChat Wed, 11/16, 2 pm ET: Industrial Energy Efficiency | Department of  

Energy.gov (U.S. Department of Energy (DOE)) Indexed Site

11/16, 2 pm ET: Industrial Energy Efficiency 11/16, 2 pm ET: Industrial Energy Efficiency LiveChat Wed, 11/16, 2 pm ET: Industrial Energy Efficiency November 14, 2011 - 1:40pm Addthis Do you have questions or ideas about how the U.S. Department of Energy can contribute to global competitiveness through industrial efficiency? Dr. Kathleen Hogan would like to hear them. Michael Hess Michael Hess Former Digital Communications Specialist, Office of Public Affairs How can I participate? Send an email to Dr. Hogan at newmedia@hq.doe.gov, tweet to @energy with the hashtag #energymatters; or leave a question on Energy's Facebook page. Throughout the last two weeks, we've been highlighting specific examples of industrial and commercial energy efficiency measures - and how they are improving American competitiveness and the economy.

434

EGYPT: The Revolution and the Future February 17, 2011, 7:30 p.m.  

E-Print Network (OSTI)

EGYPT: The Revolution and the Future February 17, 2011, 7:30 p.m. Kane Hall, Room 210 University ELLIS GOLDBERG, Professor of Political Science, University of Washington, Specialist on Egypt

Hochberg, Michael

435

AUGUST Results 31--Ohio Christian University Circleville, OH 7:00pm scrimmage  

E-Print Network (OSTI)

© Newark, OH 7:00pm W 3-0 22-- ORC State Tournament @ Ohio University Lancaster 23-- ORC State Tournament @ Ohio University Lancaster 24-- ORC State Tournament @ Ohio University Lancaster © Denotes Ohio Regional

436

Interannual Variations in PM2.5 due to Wildfires in the Western United States  

Science Journals Connector (OSTI)

Interannual Variations in PM2.5 due to Wildfires in the Western United States ... For example Craters of the Moon (CRMO1) and Bridger Wilderness (BRID1) show numerous significant correlations with sites in Colorado. ...

Dan Jaffe; William Hafner; Duli Chand; Anthony Westerling; Dominick Spracklen

2008-03-13T23:59:59.000Z

437

An Analysis of PM and NOx Train Emissions in the Alameda Corridor, CA  

E-Print Network (OSTI)

Authority. Number of Trains Running on the Alameda Corridor.An Analysis of PM and NO x Train Emissions in the Alamedaefficient than trucks, trains contribute heavily to regional

Sangkapichai, Mana; Saphores, Jean-Daniel M; Ritchie, Stephen G.; You, Soyoung Iris; Lee, Gunwoo

2008-01-01T23:59:59.000Z

438

Hangout with Clean Cities on Thursday, June 20, at 2:30 pm ET...  

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

2013 - 5:45pm Q&A Want to know what we are doing to cut the nation's oil use in transportation? Ask Us Addthis Mark your calendars for a Google+ Hangout on Clean Cities:...

439

PM Update - Steve Meador, Acting Dir for Proj Assessment-SC,...  

Energy.gov (U.S. Department of Energy (DOE)) Indexed Site

Update - Steve Meador, Acting Dir for Proj Assessment-SC, Jack Surash, Dep Asst Secretary for APM-EM, Bob Raines, Assoc. Administrator for APM-NNSA PM Update - Steve Meador, Acting...

440

Upcoming Events for November Monday, November 1, 7:30 pm  

E-Print Network (OSTI)

's All Relative - Chamber Music in Related Keys Lawrence Wheeler, viola / Frank Huang, violin Desmond 13, 7:30 pm STUDENT RECITAL - Dudley Recital Hall Katherine Svistoonoff, piano (Studio of Abbey Simon

Azevedo, Ricardo

Note: This page contains sample records for the topic "aerodynamic diameter pm" from the National Library of EnergyBeta (NLEBeta).
While these samples are representative of the content of NLEBeta,
they are not comprehensive nor are they the most current set.
We encourage you to perform a real-time search of NLEBeta
to obtain the most current and comprehensive results.


441

Mondays 2-3:30 pm, BRB 0701. Course director: Claude Krummenacher  

E-Print Network (OSTI)

Lieberman Classic: Bhende P.M., W.T. Seaman, H.J. Delecluse and S. Kenney. 2004. The EBV lytic switch and W. Hammerschmidt. 2010. CpG-Methylation Regulates a Class of Epstein-Barr Virus Promoters. PLo

Plotkin, Joshua B.

442

4:45PM ET TODAY: On-the-Record Conference Call with Administration...  

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

Initial Partners in the Better Buildings Challenge June 30, 2011 - 12:00am Addthis THE WHITE HOUSE Office of the Press Secretary WASHINGTON, D.C. - Today at 4:45PM ET, Senior...

443

2:30 PM TODAY: On-the-Record Conference Call with Deputy Assistant...  

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

Daniel Poneman to Discuss the President's Trip to Holland, Michigan to Tour the Johnson Controls I 2:30 PM TODAY: On-the-Record Conference Call with Deputy Assistant to the...

444

Condensed Matter Theory Center Wednesday, March 7, 11:00-12:30pm  

E-Print Network (OSTI)

Condensed Matter Theory Center Seminar Wednesday, March 7, 11:00-12:30pm 2205 Physics Building" Abstract: An exciting prospect in condensed matter physics is the possibility of realizing fractional

Lathrop, Daniel P.

445

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

E-Print Network (OSTI)

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

Langowski, Jörg

446

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

447

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

SciTech Connect

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.

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

2004-10-01T23:59:59.000Z

448

Journal of Wind Engineering and Industrial Aerodynamics, 30 (1988) 233-241 233 Elsevier Science Publishers B.V., Amsterdam --Printed in The Netherlands  

E-Print Network (OSTI)

Journal of Wind Engineering and Industrial Aerodynamics, 30 (1988) 233-241 233 Elsevier Science Publishers B.V., Amsterdam -- Printed in The Netherlands EFFECT OF PARAMETRIC UNCERTAINTIES ON WIND EXCITED the influence of parametric uncertainties on the wind excited response of structures. Based on the available

Kareem, Ahsan

449

Balancing Functionality with Mass Appeal in Application Development: Case Study – OneTouchPM™  

E-Print Network (OSTI)

to protect both interviewees and clients. * * * * * - 1 - Chapter 1 - Introduction In 2006 Burns & McDonnell (BMcD) was preparing for the construction phase of the largest transmission construction project in U.S. history (by dollars). The unprecedented... with project demands. 1.2 Flexibility OneTouchPM® is implemented on a project by project basis. For example, a large scale transmission line project in Oklahoma and another in California would produce two differing OneTouchPM® projects. Each...

Gepner, Christina M.

2011-05-20T23:59:59.000Z

450

Analyse Statistique de la Pollution par les PM10 en Haute-Normandie  

E-Print Network (OSTI)

Analyse Statistique de la Pollution par les PM10 en Haute-Normandie Fran¸cois-Xavier Jolloisa travail porte sur l'analyse de la pollution par les particules PM10 en r´egion Haute- Normandie entre 2004´eaires et les m´elanges de mod`eles lin´eaires, on mod´elise les effets des vari- ables sur la pollution par

Boyer, Edmond

451

#LabChat: What is Dark Energy? Oct 25 at 2pm ET | Department of Energy  

Energy.gov (U.S. Department of Energy (DOE)) Indexed Site

What is Dark Energy? Oct 25 at 2pm ET What is Dark Energy? Oct 25 at 2pm ET #LabChat: What is Dark Energy? Oct 25 at 2pm ET October 23, 2012 - 3:03pm Q&A #LabChat Oct 25, 2 pm ET | These physicists are using advanced telescopes and cameras to look for proof of dark energy. Ask them your questions. Ask Us Addthis What is dark energy? Learn about the force we think accounts for three-quarters of the mass and energy in the known universe. What is dark energy? Learn about the force we think accounts for three-quarters of the mass and energy in the known universe. Michael Hess Michael Hess Former Digital Communications Specialist, Office of Public Affairs How can I participate? Send us your questions via Twitter (@ENERGY) using #labchat. Email us your questions at newmedia@hq.doe.gov. This Thursday, October 25, at 2 p.m. EDT, three physicists studying dark

452

Characterization of particulate matter (PM10) related to surface coal mining operations in Appalachia  

Science Journals Connector (OSTI)

This study investigates the environmental exposure of residents of a community in southwest Virginia to respirable concentrations of dust (PM-10 i.e. PM10) generated by trucks hauling coal from surface coal mining operations. The study site is representative of communities in southwest Virginia and other parts of Appalachia that are located in narrow hollows where homes are placed directly along roads that experience heavy coal truck traffic. Preliminary air sampling (Particulate Matter i.e. PM10) was conducted for a period of approximately two weeks during early August 2008 in the unincorporated community of Roda, Virginia, at two locations (about a mile apart along Roda Road (Route 685) in Wise County, Virginia). For the purposes of this study (a combination of logistics, resource, and characterization of PM) we sited the PM samplers near the road to ascertain the micro exposure from the road. The results revealed high levels of PM10 (the mean adjusted 24-h concentration at the Campbell Site = 250.2 ?g m?3 (±135.0 ?g m?3); and at the Willis Site = 144.8 ± 60.0 ?g m?3). The U.S. 24-h national ambient air quality standard for PM10 is 150 ?g m?3. Elemental analysis for samples (blank-corrected) collected on Quartz filter paper (on one randomly selected day) at both the sites revealed the presence of antimony, arsenic, beryllium, cadmium, chromium, cobalt, lead, manganese, mercury, nickel, selenium. Electron micrographs reveal the morphology and habit (shapes and aggregates) of the particulate matter collected.

Viney P. Aneja; Aaron Isherwood; Peter Morgan

2012-01-01T23:59:59.000Z

453

Convective currents in nucleate pool boiling and their effects on the heat flux from varying diameter flat plate heating elements  

E-Print Network (OSTI)

investigation was conducred to amine the effects of convection currents in nucleate oool boil ing and to determine the changes in critical heat flux caused by varying the diameter of horizontal flat olate heating surfaces. Freon 113 (Trichlorotrifluoroethane... by high energy costs and thc need to economize in industrial heat transfer applications . I'nucleate boiling is a very efficient neans of heat transfer because of the large sur ace areas involved in vaporization of the bulk fluid. as bubbles form...

Morford, Peter Stephen

1980-01-01T23:59:59.000Z

454

LiveChat Wed, 6/29, 2pm: Our Energy Independence | Department of Energy  

Energy.gov (U.S. Department of Energy (DOE)) Indexed Site

LiveChat Wed, 6/29, 2pm: Our Energy Independence LiveChat Wed, 6/29, 2pm: Our Energy Independence LiveChat Wed, 6/29, 2pm: Our Energy Independence June 27, 2011 - 9:29am Addthis Ginny Simmons Ginny Simmons Former Managing Editor for Energy.gov, Office of Public Affairs How can I participate? Submit a question via E-mail, Facebook or Twitter Watch live on June 29 at 2 PM ET As many of us hit the road to celebrate America's independence this upcoming 4th of July weekend, we must once again confront the reality of our country's economy, environment and security dependence on foreign oil. On Wednesday, June 29th, at 2:00 pm ET, please join Dr. Arun Majumdar at Energy.gov for a frank, two-way discussion about the investments the federal government is making in innovative research and technology today that will move us off of foreign oil and toward the clean energy

455

Charged Higgs boson in the $W^\\pm$ Higgs channel at the Large Hadron Collider  

E-Print Network (OSTI)

In light of the recent discovery of a neutral Higgs boson, $H_{\\rm obs}$, with a mass near 125 GeV, we reassess the LHC discovery potential of a charged Higgs boson, $H^\\pm$, in the $W^\\pm H_{\\rm obs}$ decay channel. This decay channel can be particularly important for a $H^\\pm$ heavier than the top quark, when it is produced through the $pp \\rightarrow tH^\\pm$ process. The knowledge of the mass of $H_{\\rm obs}$ provides an additional handle in the kinematic selection when reconstructing a Breit-Wigner resonance in the $H_{\\rm obs} \\rightarrow b\\bar{b}$ decay channel. We consider some extensions of the Standard Model Higgs sector, with and without supersymmetry, and perform a dedicated signal-to-background analysis to test the scope of this channel for the LHC running at design energy (14 TeV), for 300/fb (standard) and 3000/fb (high) integrated luminosities. We find that, while this channel does not show much promise for a supersymmetric $H^\\pm$ state, significant portions of the parameter spaces of several ...

Enberg, Rikard; Moretti, Stefano; Munir, Shoaib; Wouda, Glenn

2014-01-01T23:59:59.000Z

456

Separate determination of PM10 emission factors of road traffic for tailpipe emissions and emissions from abrasion and resuspension processes  

Science Journals Connector (OSTI)

Little is known about the relevance of mechanically produced particles of road traffic from abrasion and resuspension processes in relation to the exhaust pipe particles. In this paper, emission factors of PM10 and PM1 for light and heavy-duty vehicles were derived for different representative traffic regimes from concentration differences of particles and nitrogen oxides (NOx) in ambient air upwind and downwind of busy roads, or alternatively of kerbsides and nearby background sites. Hereby, PM1 was interpreted as direct exhaust emissions and PM10-PM1 as mechanically produced emissions from abrasion and resuspension processes. The results show that abrasion and resuspension processes represent a significant part of the total primary PM10 emissions of road traffic. At sites with relatively undisturbed traffic flow they are in the same range as the exhaust pipe emissions. At sites with disturbed traffic flow due to traffic lights, emissions from abrasion/resuspension are even higher than those from the exhaust pipes.

Robert Gehrig; Matz Hill; Brigitte Buchmann; David Imhof; Ernest Weingartner; Urs Baltensperger

2004-01-01T23:59:59.000Z

457

Regularities of the influence of the aerodynamic coupling of blades on the formation of the spectrum of natural vibrations of the rims of turbine wheels of gas-turbine engines  

Science Journals Connector (OSTI)

We present the results of analytic and numerical investigations aimed at the evaluation of the influence of the aerodynamic coupling of blades on the formation of the spectrum of natural vibrations of the rims...

A. P. Zinkovskii; A. V. Poberezhnikov; V. A. Tsimbalyuk

2010-10-01T23:59:59.000Z

458

Supplementary information Figure S1: Left: Comparison of PM2.5 levels measured with one of the optical  

E-Print Network (OSTI)

Palau Reial L3 87 24 21 6 Bon Pastor L9 145 98 46 28 Sagrera L9 180 53 59 19 Mean Mean in trains PM10 PM10 std PM2.5 std 5min 1.20 0.22 0.43 0.10 Fontana L3 0.49 0.10 0.15 0.05 Palau Reial L3 0.30 0.08 0

Meskhidze, Nicholas

459

Program Day Date Time Room Resumes and Cover Letters Wednesday 9/3 4 p.m. 224 WPU  

E-Print Network (OSTI)

Program Day Date Time Room Resumes and Cover Letters Wednesday 9/3 4 p.m. 224 WPU Searching and Applying Friday 9/5 11 a.m. 224 WPU Networking and Social Media Friday 9/5 Noon 224 WPU Resumes and Cover Letters Tuesday 9/9 4 p.m. 540 WPU Resumes and Cover Letters Monday 9/15 4 p.m. 224 WPU Resumes and Cover

Benos, Panayiotis "Takis"

460

Hurricane Sandy Situation Report # 9 November 1, 2012 (3:00 PM EDT)  

Energy.gov (U.S. Department of Energy (DOE)) Indexed Site

9 9 November 1, 2012 (3:00 PM EDT) http://www.oe.netl.doe.gov/emergency_sit_rpt.aspx Highlights: At 8:00 pm EDT October 29, the National Hurricane Center reported Sandy made landfall near Atlantic City, NJ as a post tropical cyclone. As of 2:00 pm EDT November 1 there are 4,454,650 customers without power in the affected States. This is a decrease from the 4,657,013 customers without power reported in Situation Report #8. Restoration estimates and efforts by electric utilities are reported below. Summary Impacted State Current Customer Outages Percentage of Customers Without Power Peak Outages Reported in DOE SitReps Customers Restored Since Peak Connecticut 348,294 17% 626,559 278,265 Maryland 40,760 2% 311,020 270,260 Massachusetts 12,883 < 1% 298,072

Note: This page contains sample records for the topic "aerodynamic diameter pm" from the National Library of EnergyBeta (NLEBeta).
While these samples are representative of the content of NLEBeta,
they are not comprehensive nor are they the most current set.
We encourage you to perform a real-time search of NLEBeta
to obtain the most current and comprehensive results.


461

LiveChat Thurs, 10/20, 2pm ET: Clean Tech Markets | Department of Energy  

Energy.gov (U.S. Department of Energy (DOE)) Indexed Site

LiveChat Thurs, 10/20, 2pm ET: Clean Tech Markets LiveChat Thurs, 10/20, 2pm ET: Clean Tech Markets LiveChat Thurs, 10/20, 2pm ET: Clean Tech Markets October 17, 2011 - 11:30am Addthis Liisa O'Neill Liisa O'Neill Former New Media Specialist, Office of Public Affairs How can I participate? Send an email to newmedia@hq.doe.gov; Tweeting your question to @energy with the hashtag #energymatters; or leaving a question for Kauffman at Facebook.com/energygov. On Energy.gov, we've been showcasing a series of stories about innovations from our National Laboratories that have been successfully commercialized - and how they impact Americans' lives. During 2010 alone, our National Laboratories engaged in more than 13,500 technology transfer transactions - from licensing lab-developed technologies to using lab resources to drive industry innovation and commercial success.

462

Hurricane Sandy Situation Report # 19 November 6, 2012 (3:00 PM EST)  

Energy.gov (U.S. Department of Energy (DOE)) Indexed Site

9 9 November 6, 2012 (3:00 PM EST) http://www.oe.netl.doe.gov/emergency_sit_rpt.aspx Highlights: At 8:00 pm EDT October 29, the National Hurricane Center reported Sandy made landfall near Atlantic City, NJ as a post tropical cyclone. As of 2:00 pm EST November 6, there are 930,783 customers without power in the affected States. 7,580,468 customers have been restored out of the 8,511,251 combined total peak outages reported in the Situation Reports for all 21 States affected. Restoration estimates and efforts by electric utilities are reported below. Summary Impacted State Current Customer Outages Percentage of Customers Without Power Peak Outages Reported in DOE SitReps Customers Restored Since Peak Connecticut 7,371 < 1% 626,559 619,188 Maryland

463

Hurricane Sandy Situation Report # 1 October 28, 2012 (3:00 PM EDT)  

Energy.gov (U.S. Department of Energy (DOE)) Indexed Site

October 28, 2012 (3:00 PM EDT) http://www.oe.netl.doe.gov/emergency_sit_rpt.aspx Highlights: As of 2:00 pm EDT October 28, the National Hurricane Center reports Hurricane Sandy has maximum sustained winds of 75 mph. Sandy is 575 miles south of New York City moving northeast at 14 mph and on the forecast track the center of the storm is forecast to be near the Mid- Atlantic coast tomorrow night. As of 2:00 pm EDT October 28, there are fewer than 5,000 customers without power in Delaware, the District of Columbia, Florida, Maryland, North Carolina, South Carolina, and Virginia. Utilities are preparing for the hurricane by pre-positioning supplies, securing workers, and requesting mutual assistance support to restore power after the storm makes landfall. Restoration

464

Fourth Novatek Hammer Field Test Department of Energy Well PM-2-31  

NLE Websites -- All DOE Office Websites (Extended Search)

Novatek Hammer Field Test Novatek Hammer Field Test Department of Energy Well PM-2-31 Garfield County, Colorado September, 1995 Report Prepared for Mud Hammer Development Project Partners Mobil Oil Novatek Brian Tarr, MEPTEC Drilling MOBIL EXPLORATION AND PRODUCTION TECHNICAL CENTER Dallas, Texas September 1995 Fourth Novatek Hammer Field Test Department of Energy Well PM-2-31 September 1995 Contents Page EXECUTIVE SUMMARY 3 CONCLUSIONS 4 RECOMMENDATIONS5 5 Field Test Procedure and Results 6 APPENDIX 1 - Well Data 10 APPENDIX 2 - ∆P Calculations APPENDIX 3 - Novatek hammer drawings and photo.'s Fourth Novatek Hammer Field Test Department of Energy Well PM-2-31 September 1995 EXECUTIVE SUMMARY Objectives The primary objective of the fourth field test was to establish if the threshold level of power required to increase rock bit

465

FEDERAL ACQUISITION CERTIFICATION FOR PROGRAM AND PROJECT MANAGERS (FAC-P/PM)  

Energy.gov (U.S. Department of Energy (DOE)) Indexed Site

CERTIFICATION FOR PROGRAM AND PROJECT CERTIFICATION FOR PROGRAM AND PROJECT MANAGERS (FAC-P/PM) EXECUTIVE SUMMARY 1. Purpose. The Federal Acquisition Certification for Program and Project Managers (FAC-P/PM) establishes general training and experience requirements for program and project managers in civilian agencies. The FAC- P/PM focuses on essential competencies needed for program and project managers; the program does not include functional or technical competencies, such as those for information technology, or agency- specific competencies. 2. Background. The quality and effectiveness of the federal acquisition process depend on the development of a capable and competent workforce. The Services Acquisition Reform Act of 2003 (SARA, P.L. 108-136) expanded the definition of acquisition to include functions performed by program and project managers.

466

Earth Hour 2009: March 28, 8:30-9:30 PM Local Time | Department of Energy  

Energy.gov (U.S. Department of Energy (DOE)) Indexed Site

Earth Hour 2009: March 28, 8:30-9:30 PM Local Time Earth Hour 2009: March 28, 8:30-9:30 PM Local Time Earth Hour 2009: March 28, 8:30-9:30 PM Local Time March 27, 2009 - 6:00am Addthis John Lippert The city of Greenbelt, Maryland, where I live, is living up to its "green" name by participating in Earth Hour. This global event asks everyone to "go dark" for an hour to make a powerful statement of concern about climate change. The city will be turning off all non-essential lights in municipal buildings. Residents are requested to turn off their lights (and other energy-consuming appliances). The Greenbelt Advisory Committee on Environmental Sustainability, which advises the mayor and city council and which I chair, will be sponsoring a flashlight walk around Old Greenbelt during Earth Hour. My wife and I will

467

Earth Hour 2009: March 28, 8:30-9:30 PM Local Time | Department of Energy  

Energy.gov (U.S. Department of Energy (DOE)) Indexed Site

Earth Hour 2009: March 28, 8:30-9:30 PM Local Time Earth Hour 2009: March 28, 8:30-9:30 PM Local Time Earth Hour 2009: March 28, 8:30-9:30 PM Local Time March 27, 2009 - 6:00am Addthis John Lippert The city of Greenbelt, Maryland, where I live, is living up to its "green" name by participating in Earth Hour. This global event asks everyone to "go dark" for an hour to make a powerful statement of concern about climate change. The city will be turning off all non-essential lights in municipal buildings. Residents are requested to turn off their lights (and other energy-consuming appliances). The Greenbelt Advisory Committee on Environmental Sustainability, which advises the mayor and city council and which I chair, will be sponsoring a flashlight walk around Old Greenbelt during Earth Hour. My wife and I will

468

2:30 PM TODAY: On-the-Record Conference Call with Deputy Assistant to the  

Energy.gov (U.S. Department of Energy (DOE)) Indexed Site

:30 PM TODAY: On-the-Record Conference Call with Deputy Assistant :30 PM TODAY: On-the-Record Conference Call with Deputy Assistant to the President for Energy and Climate Change Heather Zichal and Deputy Energy Secretary Daniel Poneman to Discuss the President's Trip to Holland, Michigan to Tour the Johnson Controls I 2:30 PM TODAY: On-the-Record Conference Call with Deputy Assistant to the President for Energy and Climate Change Heather Zichal and Deputy Energy Secretary Daniel Poneman to Discuss the President's Trip to Holland, Michigan to Tour the Johnson Controls I August 10, 2011 - 11:27am Addthis WASHINGTON, D.C. - Today, Deputy Assistant to the President for Energy and Climate Change Heather Zichal and Deputy Energy Secretary Daniel Poneman will hold an on-the-record conference call to preview the President's trip tomorrow to Holland, MI to tour the Johnson Controls

469

LiveChat Thurs, 10/20, 2pm ET: Clean Tech Markets | Department of Energy  

Energy.gov (U.S. Department of Energy (DOE)) Indexed Site

LiveChat Thurs, 10/20, 2pm ET: Clean Tech Markets LiveChat Thurs, 10/20, 2pm ET: Clean Tech Markets LiveChat Thurs, 10/20, 2pm ET: Clean Tech Markets October 17, 2011 - 11:30am Addthis Liisa O'Neill Liisa O'Neill Former New Media Specialist, Office of Public Affairs How can I participate? Send an email to newmedia@hq.doe.gov; Tweeting your question to @energy with the hashtag #energymatters; or leaving a question for Kauffman at Facebook.com/energygov. On Energy.gov, we've been showcasing a series of stories about innovations from our National Laboratories that have been successfully commercialized - and how they impact Americans' lives. During 2010 alone, our National Laboratories engaged in more than 13,500 technology transfer transactions - from licensing lab-developed technologies to using lab resources to drive industry innovation and commercial success.

470

Hurricane Sandy Situation Report # 17 November 5, 2012 (3:00 PM EST)  

Energy.gov (U.S. Department of Energy (DOE)) Indexed Site

7 7 November 5, 2012 (3:00 PM EST) http://www.oe.netl.doe.gov/emergency_sit_rpt.aspx Highlights: At 8:00 pm EDT October 29, the National Hurricane Center reported Sandy made landfall near Atlantic City, NJ as a post tropical cyclone. As of 2:00 pm EST November 5, there are 1,351,683 customers without power in the affected States. 7,159,568 customers have been restored out of the 8,511,251 combined total peak outages reported in the Situation Reports for all 21 States affected. Restoration estimates and efforts by electric utilities are reported below. Summary Impacted State Current Customer Outages Percentage of Customers Without Power Peak Outages Reported in DOE SitReps Customers Restored Since Peak Connecticut 30,608 2% 626,559 595,951 Maryland

471

Hurricane Sandy Situation Report # 15 November 4, 2012 (3:00 PM EST)  

Energy.gov (U.S. Department of Energy (DOE)) Indexed Site

5 5 November 4, 2012 (3:00 PM EST) http://www.oe.netl.doe.gov/emergency_sit_rpt.aspx Highlights: At 8:00 pm EDT October 29, the National Hurricane Center reported Sandy made landfall near Atlantic City, NJ as a post tropical cyclone. As of 2:00 pm EST November 4, there are 1,855,958 customers without power in the affected States. 6,655,293 customers have been restored out of the 8,511,251 combined total peak outages reported in the Situation Reports for all 21 States affected. Restoration estimates and efforts by electric utilities are reported below. Summary Impacted State Current Customer Outages Percentage of Customers Without Power Peak Outages Reported in DOE SitReps Customers Restored Since Peak Connecticut 64,955 4% 626,559 561,604 Maryland

472

Hurricane Sandy Situation Report # 11 November 2, 2012 (3:00 PM EDT)  

Energy.gov (U.S. Department of Energy (DOE)) Indexed Site

1 1 November 2, 2012 (3:00 PM EDT) http://www.oe.netl.doe.gov/emergency_sit_rpt.aspx Highlights: At 8:00 pm EDT October 29, the National Hurricane Center reported Sandy made landfall near Atlantic City, NJ as a post tropical cyclone. As of 2:00 pm EDT November 2 there are 3,491,595 customers without power in the affected States. This is a decrease from the 3,628,739 customers without power reported in Situation Report #10. Restoration estimates and efforts by electric utilities are reported below. Summary Impacted State Current Customer Outages Percentage of Customers Without Power Peak Outages Reported in DOE SitReps Customers Restored Since Peak Connecticut 232,142 11% 626,559 394,417 Maryland 17,803 < 1% 311,020 293,217 Massachusetts 2,248 < 1% 298,072

473

Preparation of spherical fuel elements for HTR-PM in INET  

Science Journals Connector (OSTI)

Abstract The spherical fuel elements were successfully manufactured in the period of HTR-10. In order to satisfy the mass production of fuel elements for HTR-PM, several measures have been taken in modifying and optimizing the manufacture process of fuel elements. The newly developed overcoater system and its corresponding parameters exhibited good stability and high efficiency in the preparation of overcoated particles. The optimized carbonization process could reduce the carbonization time from more than 70 h to 20 h and improve the manufacturing efficiency. Properties of the manufactured spherical fuel elements and matrix graphite balls met the design specifications for HTR-PM. The mean free uranium fraction of 5 consecutive batches was 8.7 × 10?6. The optimized fuel elements manufacturing process could meet the requirements of design specifications of spherical fuel elements for HTR-PM.

Zhou Xiangwen; Lu Zhenming; Zhang Jie; Liu Bing; Zou Yanwen; Tang Chunhe; Tang Yaping

2013-01-01T23:59:59.000Z

474

From realistic 2HDM-II CPV benchmarks to the $H^\\pm \\to\\tau \  

E-Print Network (OSTI)

Phenomenological studies of a CP-violating two-Higgs-doublet Model with type-II Yukawa couplings are presented. In the light of recent LHC data, an update on the viable parameter space that survives both the experimental and theoretical constraints is provided. In addition, the scope of the LHC in exploring this model through the discovery of a charged Higgs boson that decays in the tauonic mode is analysed. For this, various production channels were investigated, with emphasis on the boson-associated channel $gg\\to H_i\\to H^\\pm W^\\mp$ and the fermion-associated channels $gb\\to H^\\pm t$ and $gg\\to H^\\pm bt$. For the latter, a signal-over-background analysis is performed.

Basso, Lorenzo; Pruna, Giovanni Marco

2014-01-01T23:59:59.000Z

475

Hurricane Sandy Situation Report # 13 November 3, 2012 (3:00 PM EDT)  

Energy.gov (U.S. Department of Energy (DOE)) Indexed Site

3 3 November 3, 2012 (3:00 PM EDT) http://www.oe.netl.doe.gov/emergency_sit_rpt.aspx Highlights: At 8:00 pm EDT October 29, the National Hurricane Center reported Sandy made landfall near Atlantic City, NJ as a post tropical cyclone. As of 2:00 pm EDT November 3 there are 2,497,421 customers without power in the affected States. 6,013,830 customers have been restored out of the 8,511,251 combined total peak outages reported in the Situation Reports for all 21 States affected. Restoration estimates and efforts by electric utilities are reported below. Summary Impacted State Current Customer Outages Percentage of Customers Without Power Peak Outages Reported in DOE SitReps Customers Restored Since Peak Connecticut 132,805 6% 626,559 493,754 Maryland

476

2:30 PM TODAY: On-the-Record Conference Call with Deputy Assistant to the  

Energy.gov (U.S. Department of Energy (DOE)) Indexed Site

2:30 PM TODAY: On-the-Record Conference Call with Deputy Assistant 2:30 PM TODAY: On-the-Record Conference Call with Deputy Assistant to the President for Energy and Climate Change Heather Zichal and Deputy Energy Secretary Daniel Poneman to Discuss the President's Trip to Holland, Michigan to Tour the Johnson Controls I 2:30 PM TODAY: On-the-Record Conference Call with Deputy Assistant to the President for Energy and Climate Change Heather Zichal and Deputy Energy Secretary Daniel Poneman to Discuss the President's Trip to Holland, Michigan to Tour the Johnson Controls I August 10, 2011 - 11:27am Addthis WASHINGTON, D.C. - Today, Deputy Assistant to the President for Energy and Climate Change Heather Zichal and Deputy Energy Secretary Daniel Poneman will hold an on-the-record conference call to preview the President's trip tomorrow to Holland, MI to tour the Johnson Controls

477

Study of Charm Fragmentation into $D^{*\\pm}$ Mesons in Deep-Inelastic Scattering at HERA  

E-Print Network (OSTI)

The process of charm quark fragmentation is studied using $D^{*\\pm}$ meson production in deep-inelastic scattering as measured by the H1 detector at HERA. Two different regions of phase space are investigated defined by the presence or absence of a jet containing the $D^{*\\pm}$ meson in the event. The parameters of fragmentation functions are extracted for QCD models based on leading order matrix elements and DGLAP or CCFM evolution of partons together with string fragmentation and particle decays. Additionally, they are determined for a next-to-leading order QCD calculation in the fixed flavour number scheme using the independent fragmentation of charm quarks to $D^{*\\pm}$ mesons.

Aaron, F D; Andreev, V; Antunovic, B; Aplin, S; Asmone, A; Astvatsatourov, A; Bacchetta, A; Backovic, S; Baghdasaryan, A; Barrelet, E; Bartel, W; Beckingham, M; Begzsuren, K; Behnke, O; Belousov, A; Berger, N; Bizot, J C; Boenig, M O; Boudry, V; Bozovic-Jelisavcic, I; Bracinik, J; Brandt, G; Brinkmann, M; Brisson, V; Bruncko, D; Bunyatyan, A; Buschhorn, G; Bystritskaya, L; Campbell, A J; Cantun Avila, K B; Cassol-Brunner, F; Cerny, K; Cerny, V; Chekelian, V; Cholewa, A; Contreras, J G; Coughlan, J A; Cozzika, G; Cvach, J; Dainton, J B; Daum, K; Deak, M; de Boer, Y; Delcourt, B; Del Degan, M; Delvax, J; De Roeck, A; De Wolf, E A; Diaconu, C; Dodonov, V; Dossanov, A; Dubak, A; Eckerlin, G; Efremenko, V; Egli, S; Eliseev, A; Elsen, E; Essenov, S; Falkiewicz, A; Faulkner, P J W; Favart, L; Fedotov, A; Felst, R; Feltesse, J; Ferencei, J; Fleischer, M; Fomenko, A; Gabathuler, E; Gayler, J; Ghazaryan, S; Glazov, A; Glushkov, I; Goerlich, L; Goettlich, M; Gogitidze, N; Gouzevitch, M; Grab, C; Greenshaw, T; Grell, B R; Grindhammer, G; Habib, S; Haidt, D; Hansson, M; Helebrant, C; Henderson, R C W; Hennekemper, E; Henschel, H; Herrera, G; Hildebrandt, M; Hiller, K H; Hoffmann, D; Horisberger, R; Hovhannisyan, A; Hreus, T; Jacquet, M; Janssen, M E; Janssen, X; Jemanov, V; Jonsson, L; Jung, Andreas Werner; Jung, H; Kapichine, M; Katzy, J; Kenyon, I R; Kiesling, C; Klein, M; Kleinwort, C; Klimkovich, T; Kluge, T; Knutsson, A; Kogler, R; Korbel, V; Kostka, P; Kraemer, M; Krastev, K; Kretzschmar, J; Kropivnitskaya, A; Kruger, K; Kutak, K; Landon, M P J; Lange, W; Lastovicka-Medin, G; Laycock, P; Lebedev, A; Leibenguth, G; Lendermann, V; Levonian, S; Li, G; Lipka, K; Liptaj, A; List, B; List, J; Loktionova, N; Lopez-Fernandez, R; Lubimov, V; Lucaci-Timoce, A I; Lytkin, L; Makankine, A; Malinovski, E; Marage, P; Marti, Ll; Martyn, H U; Maxfield, S J; Mehta, A; Meier, K; Meyer, A B; Meyer, H; Meyer, H; Meyer, J; Michels, V; Mikocki, S; Milcewicz-Mika, I; Moreau, F; Morozov, A; Morris, J V; Mozer, Matthias Ulrich; Mudrinic, M; Muller, K; Murin, P; Nankov, K; Naroska, B; Naumann, Th; Newman, Paul R; Niebuhr, C; Nikiforov, A; Nowak, G; Nowak, K; Nozicka, M; Olivier, B; Olsson, J E; Osman, S; Ozerov, D; Palichik, V; Panagoulias, I; Pandurovic, M; Papadopoulou, Th; Pascaud, C; Patel, G.D; Pejchal, O; Peng, H; Perez, E; Petrukhin, A; Picuric, I; Piec, S; Pitzl, D; Placakyte, R; Polifka, R; Povh, B; Preda, T; Radescu, V; Rahmat, A J; Raicevic, N; Raspiareza, A; Ravdandorj, T; Reimer, P; Rizvi, E; Robmann, P; Roland, B; Roosen, R; Rostovtsev, A; Rotaru, M; Ruiz Tabasco, J E; Rurikova, Z; Rusakov, S; Salek, D; Salvaire, F; Sankey, D P C; Sauter, M; Sauvan, E; Schmidt, S; Schmitt, S; Schmitz, C; Schoeffel, L; Schoning, A; Schultz-Coulon, H C; Sefkow, F; Shaw-West, R N; Sheviakov, I; Shtarkov, L N; Shushkevich, S; Sloan, T; Smiljanic, Ivan; Smirnov, P; Soloviev, Y; Sopicki, P; South, D; Spaskov, V; Specka, Arnd E; Staykova, Z; Steder, M; Stella, B; Straumann, U; Sunar, D; Sykora, T; Tchoulakov, V; Thompson, G; Thompson, P.D; Toll, T; Tomasz, F; Tran, T H; Traynor, D; Trinh, T N; Truol, P; Tsakov, I; Tseepeldorj, B; Tsurin, I; Turnau, J; Tzamariudaki, E; Urban, K; Valkarova, A; Vallee, C; Van Mechelen, P; Vargas Trevino, A; Vazdik, Y; Vinokurova, S; Volchinski, V; Wegener, D; Wessels, M; Wissing, Ch; Wunsch, E; Yeganov, V; Zacek, J; Zalesak, J; Zhang, Z; Zhelezov, A; Zhokin, A; Zhu, Y C; Zimmermann, T; Zohrabyan, H; Zomer, F; 10.1140/epjc/s10052-008-0792-2

2009-01-01T23:59:59.000Z

478

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)

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... fulfillment of the requirement for the degree of MASTER OF SCIENCE August 1969 h'h, jor Suhgect: Mechanical Engineering A SURVEY OF IDEAL FLUID PROPELLEB THEORIES AND A STUDY OF THE EFFKTS OF AERODYKVGC PROPELLER LOADING ON TRAILING VORTEX INDUCED...

Kelley, Edward Madison

2012-06-07T23:59:59.000Z

479

Determination of optimum pipe diameter along with energetic and exergetic evaluation of geothermal district heating systems: Modeling and application  

Science Journals Connector (OSTI)

This study deals with determination of optimum pipe diameters based on economic analysis and the performance analysis of geothermal district heating systems along with pipelines using energy and exergy analysis methods. In this regard, the Dikili geothermal district heating system (DGDHS) in Izmir, Turkey is taken as an application place, to which the methods presented here are applied with some assumptions. The system mainly consists of three cycles, namely (i) the transportation network, (ii) the Danistay region, and (iii) the Bariskent region. The thermal capacities of these regions are 21,025 and 7975 kW, respectively, while the supply (flow) and return temperature values of those are 80 and 50 °C, respectively. Based upon the assessment of the transportation network using the optimum diameter analysis method, minimum cost is calculated to be US$ 561856.906 year?1 for a nominal diameter of DN 300. The exergy destructions in the overall DGDHS are quantified and illustrated using exergy flow diagram. Furthermore, both energy and exergy flow diagrams are exhibited for comparison purposes. It is observed through analysis that the exergy destructions in the system particularly take place due to the exergy of the thermal water (geothermal fluid) reinjected, the heat exchanger losses, and all pumps losses, accounting for 38.77%, 10.34%, 0.76% of the total exergy input to the DGDHS. Exergy losses are also found to be 201.12817 kW and 1.94% of the total exergy input to the DGDHS for the distribution network. For the system performance analysis and improvement, both energy and exergy efficiencies of the overall DGDHS are investigated, while they are determined to be 40.21% and 50.12%, respectively.

Yildiz Kalinci; Arif Hepbasli; Ismail Tavman

2008-01-01T23:59:59.000Z

480

Optimized Use of a 50 ?m Internal Diameter Secondary Column in a Comprehensive Two-Dimensional Gas Chromatography System  

Science Journals Connector (OSTI)

Optimized Use of a 50 ?m Internal Diameter Secondary Column in a Comprehensive Two-Dimensional Gas Chromatography System ... The primary GC (GC1) was equipped with an AOC-20i autoinjector and a split?splitless injector (280 °C). ... The unmodulated applications carried out at ?15, 20, 25, 30, and 35 cm/s, analyzing a C17 alkane at an isothermal temperature of 155 °C (n = 3), generated N values of circa 122?600, 149?600, 147?600, 140?800, and 119?400, respectively. ...

Peter Quinto Tranchida; Giorgia Purcaro; Lanfranco Conte; Paola Dugo; Giovanni Dugo; Luigi Mondello

2009-09-17T23:59:59.000Z

Note: This page contains sample records for the topic "aerodynamic diameter pm" from the National Library of EnergyBeta (NLEBeta).
While these samples are representative of the content of NLEBeta,
they are not comprehensive nor are they the most current set.
We encourage you to perform a real-time search of NLEBeta
to obtain the most current and comprehensive results.


481

France to host world's first nuclear fusion plant swissinfo June 28, 2005 3:35 PM  

E-Print Network (OSTI)

France to host world's first nuclear fusion plant swissinfo June 28, 2005 3:35 PM France to host world's first nuclear fusion plant By Guy Faulconbridge MOSCOW (Reuters) - Science's quest to find-nation consortium chose France to host the world's first nuclear fusion reactor. After months

482

MAPS Executive Board Meeting Tuesday, February 26, 2013 @ 4:00pm  

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MAPS Executive Board Meeting Tuesday, February 26, 2013 @ 4:00pm MAPS Boardroom, MUSC rm 234 Call since MAPS by-law (28-a) states that the Secretary shall be the Executive Director of the MAPS. Action: Amend bi-law 28-A 3. Report/discussion items. a) A. Smith has been the primary contact for MAPS

Hitchcock, Adam P.

483

MINUTES MAPS Board Meeting April 9, 2013, MAPS Office 4-6:30pm  

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MINUTES MAPS Board Meeting April 9, 2013, MAPS Office 4-6:30pm 1 Present: J. An J. Arlen, A $133.31 to be paid to Student Financial Aid & Financial Scholarships (McMaster) b. Review of MAPS financial opportunities for students K. Pastrak was brought in to discuss the 3 MAPS awards and bursaries

Hitchcock, Adam P.

484

Sent: Thursday, October 31, 2002 9:23 PM To: Administrator Wright  

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RD-0412 Sent: Thursday, October 31, 2002 9:23 PM To: Administrator Wright Subject: Adopt the Clean for our energy supply. Why do we depend on technology that is two centuries old when we could be spending technology had improved at the same rate as computer technology Grand Coullee would be producing a glut

485

SAVE the DATE!! April 26, 2012 at 7:00 PM in Rodney Auditorium  

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of Imperial County and San Diego State University, Imperial Valley Campus For more information please visitSAVE the DATE!! April 26, 2012 at 7:00 PM in Rodney Auditorium San Diego State University Imperial Valley Campus Presentation by David Amaral, Ph.D Dealing with the heterogeneity of Autism: The Autism

Ponce, V. Miguel

486

REAL-WORLD EFFICACY OF HEAVY DUTY DIESEL TRUCK NOX AND PM EMISSIONS CONTROLS  

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are International. b DOC = Diesel Oxidation Catalyst; DPF = Diesel Particulate Filter; EGR = Exhaust GasREAL-WORLD EFFICACY OF HEAVY DUTY DIESEL TRUCK NOX AND PM EMISSIONS CONTROLS Gurdas Sandhu H 26-28, 2012 #12;2 Objectives 1. Quantify inter-run variability in exhaust emission rates 2. Assess

Frey, H. Christopher

487

K4310: Practicum in Innovative Sustainability Leadership Wed. 6:10 8 PM  

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1 SYLLABUS K4310: Practicum in Innovative Sustainability Leadership Wed. 6:10 ­ 8 PM Instructor-3871 Course Description Managers have a key role to play in advancing sustainability by integrating resource and their varied responses in the field of sustainability are covered with theory and cases in the M

488

Atmospheric Environment 39 (2005) 39673976 Seasonal trends in PM2.5 source contributions in  

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as dust (20%), secondary sulfate (17%), secondary nitrate (10%), coal combustion (7%), diesel and gasoline heating season, the contributions from coal combustion and biomass aerosol to PM2.5 mass increased of Technology, Pasadena, CA 91125, USA c Environmental Chemistry and Technology Program, University of Wisconsin

Zheng, Mei

489

Seminar Center for Advanced Vehicle Technologies Thursday, 04/29 -2:00pm  

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about on par, but when considering the power converter the up-convert architecture is best. Vehicle testSeminar ­ Center for Advanced Vehicle Technologies Thursday, 04/29 - 2:00pm 101 Bevill Hall The Role and Future of Power Electronics in Energy Storage Systems John M. Miller, PE, Ph.D. Technical

Carver, Jeffrey C.

490

Coal waste seen as valuable resource Published: March. 29, 2011 at 8:09 PM  

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Coal waste seen as valuable resource Published: March. 29, 2011 at 8:09 PM ANAHEIM, Calif., March 29 (UPI) -- Fly ash, a byproduct of coal-burning electric power plants, could save billions. More than 450 coal-burning electric power plants in the United States produce about 130 million tons

Belogay, Eugene A.

491

4-H Marine Camp! June 18th and 19th, 9am-3pm  

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4-H Marine Camp! June 18th and 19th, 9am-3pm Are you interested in Marine Ecology? 4-H will be hosting a Marine Day Camp on Tuesday, June 18th and Wednesday, June 19th. Day 1 will be located......................... 9) Hypoglycemia.................... 10) Serious Insect Stings............ 11) Wear Glasses

Watson, Craig A.

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Wed., January 30 | noon -1:00p.m. King Hall, Room 1002  

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, Moskovitz, Tiedemann & Girard. Saracino earned her law degree from UC Davis School of Law, and has a bachelor of arts degree in economics from UC Davis. Wed., march 27 | noon - 1:00p.m. King Hall, Room 1002's office as a Supervising Deputy Attorney General on the Energy Task Force, representing the state

California at Davis, University of

493

Position Description Report Run Date Aug 28 2013 2:46PM  

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of analysis, design, implementation, testing, and integration of applications supported by EAISPosition Description Report Run Date Aug 28 2013 2:46PM Position Number: TBD Dept: IET APPLICATION DEVELOPMENT - 061419 Position: APPLICATION DEVELOPER Approved Payroll Title Code: TBD Approved Payroll Title

California at Davis, University of

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Taylor relaxation and decay of unbounded, freely-expanding J. Yee and P.M. Bellan  

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Taylor relaxation and ¸ decay of unbounded, freely-expanding spheromaks J. Yee and P.M. BellanJÁ=BÁ indicate that the spheromak is decaying and expanding in a manner analogous to a self's relaxation model [1,2] has been successfully applied to many fusion related plasmas, especially spheromaks

Bellan, Paul M.

495

High Current Effects in Silicide Films for Sub-0.25 pm VLSI Technologies  

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to the increased use of silicided metalization schemes for low-resistivity gates, interconnections and contacts between the metal and Si. Currently, self aligned silicide (salicide) processes are widely usedHigh Current Effects in Silicide Films for Sub-0.25 pm VLSI Technologies Kaustav Banerjee

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Modeling Icon Search in ACT-R/PM Michael D. Fleetwood and Michael D. Byrne  

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Modeling Icon Search in ACT-R/PM Michael D. Fleetwood and Michael D. Byrne {fleet, byrne As the use of graphical user interfaces expands into new areas, icons are becoming an increasingly important with using icons. One aspect of icons, icon borders, has been proposed as a means of adding information

Byrne, Mike

497

Energy and Energy Policy by Steve Berry on September 29th, 2008, 1:37 pm  

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Energy and Energy Policy by Steve Berry on September 29th, 2008, 1:37 pm 29 September 2008 candidates. I say this as a scientist who has spent much of my research life studying energy, including energy efficiency, and environment. I've taught courses for years on energy and environmental management

Berry, R. Stephen

498

Sent: Thursday, September 26, 2002 8:01 PM To: Comment@bpa.gov  

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RD-0146 Sent: Thursday, September 26, 2002 8:01 PM To: Comment@bpa.gov Subject: Salmon Dear salmon, clean, renewable energy, and a healthy economy. The Bonneville Power Administration (BPA and Snake rivers, which will have profound impacts on salmon and salmon dependent communities. To date, BPA

499

Sent: Tuesday, October 08, 2002 11:13 PM To: comment@bpa.gov  

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RD-0290 Sent: Tuesday, October 08, 2002 11:13 PM To: comment@bpa.gov Subject: BPA should promote dependent communities. Under the status quo, BPA and other federal agencies have largely failed to meet their legal salmon recovery responsibilities. I urge the Bonneville Power Administration (BPA) to ensure

500

Sent: Tuesday, September 24, 2002 5:52 PM To: comment@bpa.gov  

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RD-0131 Sent: Tuesday, September 24, 2002 5:52 PM To: comment@bpa.gov Subject: Salmon & Power Dear Administrator Wright, I understand that the BPA is undergoing discussions to make changes to power distribution changes continue, I hope that BPA makes it a priority to improve the conditions of wild salmon, as well