Influence of boundary conditions relaxation on panel flutter with compressive in-plane loads

Journal of Fluids and Structures

Volumn 21, Issue 8, 2005, Pages 743-767

  Beloiu, D M ^a   Ibrahim, Raouf A ^a   Pettit, C L ^b  

^a Wayne State University   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC LOADS; AIRCRAFT PARTS AND EQUIPMENT; BOUNDARY CONDITIONS; BOUNDARY VALUE PROBLEMS; EQUATIONS OF MOTION; FLUID STRUCTURE INTERACTION; FOURIER TRANSFORMS; FREQUENCY DOMAIN ANALYSIS; GALERKIN METHODS; ORDINARY DIFFERENTIAL EQUATIONS; PARTIAL DIFFERENTIAL EQUATIONS; TIME DOMAIN ANALYSIS;

BOUNDARY CONDITIONS RELAXATION; PANEL FLUTTER; SPECIAL COORDINATE TRANSFORMATION;

FLUTTER (AERODYNAMICS);

BIFURCATION; BOUNDARY CONDITIONS; FLUID-STRUCTURE INTERACTION; FLUTTER;

EID: 28744445660     PISSN: 08899746     EISSN: 10958622     Source Type: Journal    
DOI: 10.1016/j.jfluidstructs.2005.07.007     Document Type: Article

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