An efficient method for nonlinear aeroelasticy of slender wings

Nonlinear Dynamics

Volumn 67, Issue 1, 2012, Pages 659-681

  Shams, S ^a   Sadr, M H ^a   Haddadpour, H ^b  

^a AMIRKABIR UNIVERSITY OF TECHNOLOGY   (Iran)

^b SHARIF UNIVERSITY OF TECHNOLOGY   (Iran)

Author keywords

High aspect ratio wings; Mode summation method; Nonlinear beam equations; Unsteady aerodynamic

Indexed keywords

AERODYNAMIC LOADING; AEROELASTIC RESPONSE; EULER-BERNOULLI BEAM EQUATION; FLIGHT OPERATION; GALERKIN'S METHOD; GOVERNING EQUATIONS; HIGH ASPECT RATIO; HIGH-ASPECT RATIO WING; LARGE DEFLECTION; LINEAR AERODYNAMICS; MODE SUMMATION METHOD; NONLINEAR AEROELASTIC ANALYSIS; NONLINEAR BEAM EQUATION; SLENDER WINGS; STATE SPACE; STRIP THEORY; STRUCTURAL MODELING; STRUCTURAL MODELS; TEST CASE; THIRD-ORDER; UNSTEADY AERODYNAMICS; WING FLEXIBILITY;

AERODYNAMICS; AEROELASTICITY; ASPECT RATIO; CONTINUUM MECHANICS; EULER EQUATIONS; FLEXIBLE WINGS; GALERKIN METHODS; MODEL STRUCTURES; NUMERICAL METHODS;

NONLINEAR EQUATIONS;

EID: 82255175326     PISSN: 0924090X     EISSN: None     Source Type: Journal    
DOI: 10.1007/s11071-011-0018-2     Document Type: Article

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