Aerothermodynamic testing and boundary layer trip sizing of the HIFiRE flight 1 vehicle

46th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2008, Pages

  Berger, Karen T ^a   Greene, Frank A ^a   Kimmel, Roger ^b  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ANGLES OF ATTACK; EXPERIMENTAL DATA; EXPERIMENTAL MEASUREMENTS; FLIGHT EXPERIMENTS; FLIGHT-TEST VEHICLES; HEAT TRANSFER DISTRIBUTIONS; HEAT TRANSFER MODEL; INTERNATIONAL FLIGHTS; NASA LANGLEY RESEARCH CENTER; PHOSPHOR THERMOGRAPHY; TEST REPORTS; WIND TUNNEL TESTS;

AEROSPACE ENGINEERING; EXPERIMENTS; HEAT TRANSFER; NASA; REYNOLDS NUMBER; WIND TUNNELS;

BOUNDARY LAYERS;

EID: 78149463014     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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