Nonlinear aeroelastic modeling and analysis of fully flexible aircraft

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

Volumn 7, Issue , 2005, Pages 4472-4498

  Cesnik, Carlos E S ^a,b,c   Su, Weihua ^a,b  

^a UNIVERSITY OF MICHIGAN   (United States)

^b Department of Aerospace Engineering ^*  (United States)

^c AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; DEFLECTION (STRUCTURES); FINITE ELEMENT METHOD; FUSELAGES; LINEAR SYSTEMS; ROTATION; SENSORS; STATE SPACE METHODS; SUBSONIC AERODYNAMICS;

CROSS-SECTIONAL STIFFNESS; FLEXIBLE AIRCRAFTS; NONLINEAR AEROELASTIC MODELING; STATE SPACE AEROELASTIC MODELS;

AERODYNAMICS;

EID: 28844460033     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2005-2169     Document Type: Conference Paper

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