skip to main content
OSTI.GOV title logo U.S. Department of Energy
Office of Scientific and Technical Information

Title: CUAS T&E Methodology.

Abstract

Abstract not provided.

Authors:
; ;
Publication Date:
Research Org.:
Sandia National Lab. (SNL-NM), Albuquerque, NM (United States)
Sponsoring Org.:
USDOE National Nuclear Security Administration (NNSA)
OSTI Identifier:
1431655
Report Number(s):
SAND2017-3859C
652436
DOE Contract Number:
AC04-94AL85000
Resource Type:
Conference
Resource Relation:
Conference: Proposed for presentation at the SPIE DCS held April 9-15, 2017 in Anaheim, CA.
Country of Publication:
United States
Language:
English

Citation Formats

Kouhestani, Camron G, Woo, Bryana Lynn, and Birch, Gabriel Carlisle. CUAS T&E Methodology.. United States: N. p., 2017. Web.
Kouhestani, Camron G, Woo, Bryana Lynn, & Birch, Gabriel Carlisle. CUAS T&E Methodology.. United States.
Kouhestani, Camron G, Woo, Bryana Lynn, and Birch, Gabriel Carlisle. Sat . "CUAS T&E Methodology.". United States. doi:. https://www.osti.gov/servlets/purl/1431655.
@article{osti_1431655,
title = {CUAS T&E Methodology.},
author = {Kouhestani, Camron G and Woo, Bryana Lynn and Birch, Gabriel Carlisle},
abstractNote = {Abstract not provided.},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {Sat Apr 01 00:00:00 EDT 2017},
month = {Sat Apr 01 00:00:00 EDT 2017}
}

Conference:
Other availability
Please see Document Availability for additional information on obtaining the full-text document. Library patrons may search WorldCat to identify libraries that hold this conference proceeding.

Save / Share:
  • Abstract not provided.
  • Abstract not provided.
  • Simulation of hypersonic flight in ground test and evaluation (T and E) facilities is a challenging and formidable task, especially to fully duplicate the flight environment above approximately Mach 8 for most all hypersonic flight systems that have been developed, conceived, or envisioned. Basically, and for many years, the enabling technology to build such a ground test wind tunnel facility has been severely limited in the area of high-temperature, high-strength materials and thermal protection approaches. To circumvent the problems, various approaches have been used, including partial simulation and use of similarity laws and reduced test time. These approaches often aremore » not satisfactory, i.e. operability and durability testing for air-breathing propulsion development and thermal protection development of many flight systems. Thus, there is a strong need for science and technology (S and T) community involvement in technology development to address these problems. This paper discusses a specific case where this need exists and where significant S and T involvement has made and continues to make significant contributions. The case discussed will be an Air Force research program currently underway to develop enabling technologies for a Mach 8-15 hypersonic true temperature wind tunnel with relatively long run time. The research is based on a concept proposed by princeton University using radiant or beamed energy into the supersonic nozzle flow.« less
  • Abstract not provided.
  • Abstract not provided.