Integrated approach to assessment of transonic abrupt wing stall for advanced aircraft

Journal of Aircraft

Volumn 42, Issue 3, 2005, Pages 646-652

  Cook, Stephen P ^a   Kokolios, Alexander ^a   Page, Anthony ^a   Chambers, Joseph ^b   Niewoehner, Robert ^c   Owens, D Bruce ^d   Roesch, Michael ^e  

^a NAVAL AIR SYSTEMS COMMAND   (United States)

^b Ball Corporation   (United States)

^c UNITED STATES NAVAL ACADEMY   (United States)

^d NASA LANGLEY RESEARCH CENTER   (United States)

^e BOEING COMPANY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACCIDENT PREVENTION; AERODYNAMICS; AIRCRAFT; DAMPING; MACHINE DESIGN; RESEARCH; WINGS;

AIRCRAFT DESIGN; PROGRAM MANAGER; TRANSONIC ABRUPT WING STALL;

COMPUTATIONAL FLUID DYNAMICS;

EID: 22544447817     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.2834     Document Type: Article

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