Nonlinear aeroelastic response of the flexible wing in trim

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

Volumn 1, Issue , 2006, Pages 436-455

  Nichkawde, Chetan ^a   Strganac, Thomas W ^a,c,d   Beran, Philip S ^b,d  

^a TEXAS A AND M UNIVERSITY   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

^c TAMU 3141

^d AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; ANGLE OF ATTACK; ASPECT RATIO; BIFURCATION (MATHEMATICS); COMPUTER SIMULATION; DYNAMIC RESPONSE; WINGS;

IN-PLANE MOTION; NONLINEAR AEROELASTIC RESPONSE; QUASI-STEADY APPROACH; TRIM CONDITIONS;

NONLINEAR SYSTEMS;

EID: 34247096112     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2006-1637     Document Type: Conference Paper

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