Nonlinear aeroelastic formulation for flexible high-aspect ratio wings via geometrically exact approach

Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference

Volumn , Issue , 2011, Pages

  Arena, Andrea ^a   Lacarbonara, Walter ^a   Marzocca, Pier ^b  

^a SAPIENZA UNIVERSITY OF ROME   (Italy)

^b Clarkson University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERO-ELASTIC SIMULATIONS; AEROELASTIC BEHAVIOR; BEDDOES-LEISHMAN MODEL; DYNAMIC STALLS; EQUATION OF MOTION; FLUTTER BOUNDARIES; FULLY NONLINEAR; GEOMETRICALLY EXACT; GOVERNING EQUATIONS; HIGH-ASPECT RATIO WING; HYBRID SOLUTION; LARGE DEFORMATIONS; NON-LINEAR PHENOMENA; NONLINEAR AEROELASTIC MODELING; NUMERICAL INTEGRATIONS; NUMERICAL INVESTIGATIONS; NUMERICAL SCHEME; REDUCED ORDER; SPACE AND TIME; STRUCTURAL MODELS; UNSTEADY AERODYNAMIC LOAD; UNSTEADY AERODYNAMICS; VISCOUS EFFECT;

AERODYNAMIC STALLING; AEROELASTICITY; ASPECT RATIO; EQUATIONS OF MOTION; MODEL STRUCTURES; NUMERICAL METHODS; STRUCTURAL DYNAMICS; THREE DIMENSIONAL;

FLEXIBLE WINGS;

EID: 84872454271     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2011-1916     Document Type: Conference Paper

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