CFD analysis of the flow around the X-31 aircraft at high angle of attack

Collection of Technical Papers - AIAA Applied Aerodynamics Conference

Volumn , Issue , 2009, Pages

  Boelens, O J ^a  

^a NATIONAL AEROSPACE LABORATORY NLR   (Netherlands)

Author keywords

[No Author keywords available]

Indexed keywords

ANGLE OF ATTACK; ANGLE OF ATTACK INDICATORS; COMPUTATIONAL FLUID DYNAMICS; COST EFFECTIVENESS; FIGHTER AIRCRAFT; FLIGHT CONTROL SYSTEMS; FLOW SIMULATION; RESEARCH AIRCRAFT;

COMPUTATIONAL FLUID DYNAMICS METHODS; HIGH ANGLE OF ATTACK; LOW-SPEED WIND TUNNEL; NATIONAL AEROSPACE LABORATORIES; PITCHING MOMENT COEFFICIENTS; STABILITY AND CONTROL; WIND TUNNEL EXPERIMENT; WIND TUNNEL MODELING;

WIND TUNNELS;

EID: 85067320294     PISSN: 10485953     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2009-3628     Document Type: Conference Paper

References (14)

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