Comparison of HYPER-X Mach 10 scramjet preflight predictions and flight data

A Collection of Technical Papers - 13th AIAA/CIRA International Space Planes and Hypersonic Systems and Technologies Conference

Volumn 2, Issue , 2005, Pages 1412-1418

  Ferlemann, Paul G ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

FLIGHT DATA; FLIGHT TESTS; SCRAMJETS; TUNNEL TESTING;

COMPUTATIONAL FLUID DYNAMICS; DATABASE SYSTEMS; FLIGHT DYNAMICS; HYPERSONIC AERODYNAMICS; JET ENGINES; WIND TUNNELS;

JETS;

EID: 29044433676     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (8)

1. th International Space Planes and Hypersonics Systems & Technology Conference, Norfolk, VA, 18-22 November 1996.
2. Pinckney, S.Z., Ferlemann,S.M., Mills, J.C., and Bass, L.S., "Program Manual for SRGULL version 2.0," HYPER-X Program Office Document HX-829.1, December 2004.
3. McGrory, W.D., Slack, D.C., Applebaum, M.P., and Walters, R.W., GASP Version 2.2, The General Aerodynamic Simulation Program, Aerosoft Inc., 1993.
4. Kamath, P.S., Mao, M.M., and McClinton, C.R., "Scramjet Combustor Analysis with the SHIP3D PNS Code," AIAA Paper 1991-5090.
5. Bakos, R.J., Tsai, C-Y., Rogers, R.C., and Shih, A.T., "The Mach 10 Component of NASA's HYPER-X Ground Test Program," ISABE-99-7216, September, 1999.
6. th International Space Planesand Hypersonic Systems and Technologies Conference, Kyoto, Japan, 24-27 April 2001.
7. th Joint Propulsion Conference, Salt Lake City, Utah, 9-11 July 2001.
8. Rogers, R.C., Shih, A.T., and Hass, N.B., "Scramjet Development Tests Supporting the Mach 10 Flight of the X-43," AIAA Paper 2005-3351.