High fidelity computational simulation of a membrane wing airfoil

46th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2008, Pages

  Gordnier, Raymond E ^a  

^a AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRFOILS; ANGLE OF ATTACK; CAMBERS; DRAG; FLEXIBLE WINGS; NAVIER STOKES EQUATIONS; REYNOLDS NUMBER;

COMPUTATIONAL SIMULATION; DYNAMIC STRUCTURAL RESPONSE; FLEXIBLE MEMBRANES; HIGH ANGLES OF ATTACK; LOW REYNOLDS NUMBER; NAVIER-STOKES SOLVER; NONLINEAR STRUCTURAL RESPONSE; STRUCTURAL MODELING;

MEMBRANES;

EID: 78149438723     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2008-614     Document Type: Conference Paper

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