Poststall prediction of multiple-lifting-surface configurations using a decambering approach

Journal of Aircraft

Volumn 43, Issue 3, 2006, Pages 660-668

  Mukherjee, Rinku ^a,b,c,d   Gopalarathnam, Ashok ^a,b,d  

^a NORTH CAROLINA STATE UNIVERSITY   (United States)

^b Department of Mechanical and Aerospace Engineering ^*  (United States)

^c MV Systems Inc   (United States)

^d AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; CONVERGENCE OF NUMERICAL METHODS; NEWTONIAN FLOW; STABILITY; VORTEX FLOW;

AIRCRAFT STABILITY; ITERATIVE DECAMBERING APPROACH; LIFTING-LINE; POSTSTALL CONDITIONS;

ITERATIVE METHODS;

EID: 33746114869     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.15149     Document Type: Article

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