Time domain nonlinear aeroelastic analysis for HALE wings

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

Volumn 1, Issue , 2006, Pages 488-506

  Wang, Z ^a,c   Chen, P C ^a,c   Liu, D D ^a,c   Mook, D T ^b,d   Patil, M J ^b,d  

^a ZONA TECHNOLOGY INC   (United States)

^b VIRGINIA POLYTECHNIC INSTITUTE AND STATE UNIVERSITY   (United States)

^c AIAA   (United States)

^d Dept of Engineering Science and Mechanics ^*

Author keywords

[No Author keywords available]

Indexed keywords

FLIGHT LOADS; HIGH ALTITUDE LONG ENDURANCE (HALE) AIRCRAFT; NONLINEAR BEAM; NONLINEAR VORTEX-LATTICE METHOD (UVLM);

ANISOTROPY; FINITE ELEMENT METHOD; MATHEMATICAL MODELS; NONLINEAR SYSTEMS; TIME DOMAIN ANALYSIS; WINGS;

AERODYNAMICS;

EID: 34247106288     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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