Effects of structural nonlinearity on subsonic aeroelastic characteristics of an aircraft wing with control surface

Journal of Fluids and Structures

Volumn 19, Issue 6, 2004, Pages 747-763

  Bae, J S ^a   Inman, D J ^a   Lee, I ^b  

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

^b Korea Advanced Institute of Science and Technology (KAIST)   (South Korea)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; APPROXIMATION THEORY; FINITE ELEMENT METHOD; SUBSONIC AERODYNAMICS;

AERODYNAMIC FORCES; MINIMUM-STATE APPROXIMATION; PERIODIC MOTIONS;

WINGS;

AERODYNAMIC FORCE; AEROELASTICITY; FLUID-STRUCTURE INTERACTION; FLUTTER; NON-LINEAR DYNAMICS; WING;

EID: 3042820279     PISSN: 08899746     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.jfluidstructs.2004.04.005     Document Type: Article

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