Implicit LES simulations of a low Reynolds number flexible membrane wing airfoil

47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition

Volumn , Issue , 2009, Pages

  Gordnier, Raymond E ^a   Attar, Peter J ^b  

^a AIR FORCE RESEARCH LABORATORY   (United States)

^b UNIVERSITY OF OKLAHOMA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRFOILS; ANGLE OF ATTACK; FLEXIBLE WINGS; NAVIER STOKES EQUATIONS; ONE DIMENSIONAL; REYNOLDS NUMBER; STRUCTURAL DYNAMICS;

COMPUTATIONAL RESULTS; EXPERIMENTAL CHARACTERIZATION; FINITE-ELEMENT APPROACH; FLEXIBLE MEMBRANES; LOW REYNOLDS NUMBER; NAVIER-STOKES SOLVER; STRUCTURAL MODELING; STRUCTURAL RESPONSE;

MEMBRANES;

EID: 78649312642     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2009-579     Document Type: Conference Paper

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