Calculation of airfoil flutter by an Euler method with approximate boundary conditions

16th AIAA Computational Fluid Dynamics Conference

Volumn , Issue , 2003, Pages

  Gao, C ^a   Luo, S ^a   Liu, F ^a   Schuster, D M ^b  

^a University of California at Irvine   (United States)

^b NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRFOILS; ANGLE OF ATTACK; COMPUTATIONAL FLUID DYNAMICS; DEFORMATION; EULER EQUATIONS; FLUID STRUCTURE INTERACTION; FLUTTER (AERODYNAMICS); NONLINEAR EQUATIONS; NUMERICAL METHODS; SHOCK WAVES;

APPROXIMATE BOUNDARY CONDITION; EFFICIENT NUMERICAL METHOD; FLUID-STRUCTURE INTERACTION PROBLEM; FLUTTER BOUNDARIES; NONLINEAR EULER EQUATIONS; SMALL DEFORMATIONS; UNSTEADY EULER EQUATIONS; WALL BOUNDARY CONDITION;

BOUNDARY CONDITIONS;

EID: 85087190272     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2003-3830     Document Type: Conference Paper

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