From water tunnel to post-stall flight simulation - The F/A-18 investigation (invited)

40th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2002, Pages

  Beyers, Martin E ^a  

^a NATIONAL RESEARCH COUNCIL CANADA   (Canada)

Author keywords

[No Author keywords available]

Indexed keywords

BOMBERS; DATA VISUALIZATION; DELTA WING AIRCRAFT; FLIGHT SIMULATORS; HYDRAULIC STRUCTURES; REYNOLDS NUMBER; SUPERSONIC AIRCRAFT; TUNNELS; VORTEX FLOW; WATER SUPPLY TUNNELS; WINGS;

AIRCRAFT CONFIGURATIONS; FLIGHT SIMULATION; FLIGHT SIMULATION MODELS; HIGH ALPHA AERODYNAMICS; HIGH SENSITIVITY; SIMULATOR DATABASE; VORTEX BREAKDOWN; WATER TUNNEL EXPERIMENTS;

AERODYNAMICS;

EID: 85088722455     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2002-699     Document Type: Conference Paper

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