Hypersonic boundary-layer trip development for hyper-X

Journal of Spacecraft and Rockets

Volumn 38, Issue 6, 2001, Pages 853-864

  Berry, Scott A ^a,d   Auslender, Aaron H ^a,e   Dilley, Arthur D ^b,f   Calleja, John F ^c,g  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b FDC/NYMA   (United States)

^c General Applied Sciences Laboratory Inc   (United States)

^d Aerothermodynamics Branch   (United States)

^e Hypersonic Airbreathing Propulsion Branch   (United States)

^f RAYTHEON COMPANY   (United States)

^g AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT PROPULSION; AIRFRAMES; BOUNDARY LAYERS; COMPUTATIONAL FLUID DYNAMICS; COMPUTER SIMULATION; HEAT TRANSFER; PHOSPHORS; RESEARCH AIRCRAFT; REYNOLDS NUMBER; THERMOGRAPHY (TEMPERATURE MEASUREMENT); THIN FILMS; WIND TUNNELS;

AIR TUNNELS; AIRFRAME INTEGRATED SCRAMJET PROPULSION; PHOSPHOR THERMOGRAPHY; REFLECTED SHOCK TUNNEL;

HYPERSONIC AERODYNAMICS;

EID: 0035518402     PISSN: 00224650     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.3775     Document Type: Article

References (52)

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