Flight data analysis of HyShot 2

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

Volumn 2, Issue , 2005, Pages 1429-1445

  Mass, Neal E ^a,c   Smart, Michael K ^a,c   Paull, Allan ^b,d  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b UNIVERSITY OF QUEENSLAND   (Australia)

^c Hypersonic Airbreathing Propulsion Branch   (United States)

^d Mechanical Engineering Department

Author keywords

[No Author keywords available]

Indexed keywords

DOUBLE WEDGE; GROUND TESTS; SCRAMJETS; SUPERSONIC COMBUSTION;

APPROXIMATION THEORY; DATA REDUCTION; HYDROGEN FUELS; JETS; LAUNCHING; REENTRY; VEHICLES;

FLIGHT DYNAMICS;

EID: 29044432591     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (8)

1. Curran, E.T.,"Scramjet Engines: The First Forty Years", Journal of Propulsion and Power, Vol 17, No. 6., pp1138-1148, 2001.
2. Guy, R.W., Rogers, R.C., Puster, R.L., Rock, K.E. and Diskin, G.S., "The NASA Langley Scramjet Test Complex", AIAA 96-3243, July, 1996.
3. Paull, A., Stalker, R.J. and Mee, D.J, 1995, "Experiments on supersonic combustion ramjet propulsion in a shock tunnel", J. Fluid Mech vol 296 pp159-183.
4. Paull, A., Alesi, H. and Anderson, S., "HyShot Flight Program and how it was developed", AIAA 02-4939, September 2002.
5. Paull, A., Frost, M. and Alesi, H., "HyShot-T4 Supersonic Combustion Experiments", report for NAG-1-2113, 2000.
6. Cain, T., Owens, R. and Walton, C., "Reconstruction of the HyShot 2 Flight from Onboard Sensors" Fifth Symposium on Aerothermodynamics for Space Vehicles, Cologne, Germany, November 2004.
7. Owens, R. and Cain, T., "HyShot 2 Aerodynamics", Fifth Symposium on Aerothermodynamics for Space Vehicles, Cologne, Germany, November 2004.
8. Tatum, K.E., "Computation of thermally perfect properties of oblique shock waves", NASA CR 4749, 1996.