Wind tunnel testing, flight scaling and flight validation with hyper-X

20th AIAA Advanced Measurement and Ground Testing Technology Conference

Volumn , Issue , 1998, Pages

  McClinton, C R ^a   Voland, R T ^a   Holland, S D ^a   Engelund, W C ^a   White, J T ^b   Pahle, J W ^b  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b NASA DRYDEN FLIGHT RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRFRAMES; COMBUSTION; FLIGHT DYNAMICS; FLIGHT SIMULATORS; NASA; NUMERICAL METHODS; PROPULSION; SOFTWARE TESTING; STRUCTURAL FRAMES; SUPERSONIC AIRCRAFT; UNMANNED VEHICLES; VEHICLES; WIND STRESS;

AIR BREATHING VEHICLES; DATABASE DEVELOPMENT; HYPERSONIC TECHNOLOGY; LABORATORY ENVIRONMENT; LANGLEY RESEARCH CENTERS; PERFORMANCE VALIDATION; PROTOTYPE DEVELOPMENT; SUPERSONIC COMBUSTION;

WIND TUNNELS;

EID: 84982318940     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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