Aerodynamic database development for the Hyper-X airframe-integrated scramjet propulsion experiments

Journal of Spacecraft and Rockets

Volumn 38, Issue 6, 2001, Pages 803-810

  Engelund, Walter C ^a   Holland, Scott D ^a   Cockrell Jr , Charles E ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT PROPULSION; AIRFRAMES; BOOSTERS (ROCKET); COMPUTATIONAL FLUID DYNAMICS; EQUIPMENT TESTING; FLIGHT DYNAMICS; HYPERSONIC AERODYNAMICS; RAMJET ENGINES; STABILITY; WIND TUNNELS;

AERODYNAMIC DATABASE; AIRFRAME INTEGRATED SCRAMJET PROPULSION ENGINE; FLIGHT TESTS; SCRAMJET ENGINE TEST; WIND TUNNEL TEST;

RESEARCH AIRCRAFT;

EID: 0035518190     PISSN: 00224650     EISSN: 15336794     Source Type: Journal    
DOI: 10.2514/2.3768     Document Type: Article

References (21)

1. NASA scramjet flight to breath new life into hypersonics
2. Hyper-X: Flight validation of hypersonic airbreathing technology
3. Hyper-X flight engine ground testing for flight risk reduction
4. Hyper-X stage separation wind-tunnel test program
5. Computational fluid dynamics prediction of hyper-X stage separation aerodynamics
6. Hyper-X research vehicle experimental aerodynamics test program overview
7. Integrated aeropropulsive computational fluid dynamics methodology for the hyper-X flight experiment
8. Hypersonic boundary-layer trip development for hyper-X