Modeling aerodynamic nonlinearities for two aeroelastic configurations: Delta wing and flapping flag

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

Volumn 1, Issue , 2003, Pages 12-22

  Attar, Peter J ^a   Dowell, Earl H ^a   Tang, Deman ^a  

^a NONE

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY CONDITIONS; COMPUTER SIMULATION; EQUATIONS OF MOTION; FINITE ELEMENT METHOD; FLUTTER (AERODYNAMICS); HAMILTONIANS; LINEAR EQUATIONS; MATHEMATICAL MODELS; VORTEX FLOW; WAKES; WINGS;

AERODYNAMIC NONLINEARITIES; ANGLES OF ATTACK; DELTA WING; FLAPPING FLAG; LIMIT CYCLE OSCILLATION; NONLINEAR AERODYNAMIC MODEL; NONLINEAR STRUCTURAL MODEL; UNSTEADY VORTEX LATTICE THEORY;

AERODYNAMICS;

EID: 0041513000     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2003-1402     Document Type: Conference Paper

References (14)

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