Effects of geometric structural nonlinearity of flutter and limit cycle oscillations of high-aspect-ratio wings

Journal of Fluids and Structures

Volumn 19, Issue 3, 2004, Pages 291-306

  Tang, D M ^a   Dowell, E H ^a  

^a DUKE UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ASPECT RATIO; FLUTTER (AERODYNAMICS); GRAVITATION; OSCILLATIONS; PARAMETER ESTIMATION; PERTURBATION TECHNIQUES; DEFORMATION; MATHEMATICAL MODELS; NONLINEAR EQUATIONS; WINGS;

LIMIT CYCLE OSCILLATIONS (LCO); NONLINEAR BEAM THEORY; NONLINEAR FORCES; STRUCTURAL EQUATIONS;

EQUATIONS OF MOTION; FLUTTER (AERODYNAMICS);

AERODYNAMICS; FLOW VELOCITY; FLUID-STRUCTURE INTERACTION; FLUTTER; NON-LINEAR MOTION; WING; OSCILLATION;

NONLINEAR BEAM THEORY; STRUCTURAL EQUATIONS;

EID: 3042590364     PISSN: 08899746     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.jfluidstructs.2003.10.007     Document Type: Article

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