Transonic free-to-roll analysis of abrupt wing stall on military aircraft

Journal of Aircraft

Volumn 41, Issue 3, 2004, Pages 474-484

  Owens, D Bruce ^a   Capone, Francis J ^a   Hall, Robert M ^a   Brandon, Jay M ^a   Chambers, Joseph R ^b  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b Ball Aerospace Systems Division   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACCELERATION; DAMPING; REYNOLDS NUMBER; ROLLING; TRANSONIC AERODYNAMICS; VELOCITY MEASUREMENT; WIND TUNNELS;

ABRUPT WING STALL (AWS); FREE-TO-ROLL ANALYSIS; ROLL DAMPING; TRANSONIC SPEEDS;

MILITARY AIRCRAFT;

EID: 3042756739     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.3073     Document Type: Review

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