Linear and nonlinear aeroelastic analysis of fighter-type wing with control surface

Journal of Aircraft

Volumn 39, Issue 4, 2002, Pages 697-708

  Bae, Jae Sung ^a   Yang, Seung Man ^a   Lee, In ^a  

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

Author keywords

[No Author keywords available]

Indexed keywords

CHAOS THEORY; COMPUTATION THEORY; FLUTTER (AERODYNAMICS); FREQUENCY DOMAIN ANALYSIS; OSCILLATIONS; TIME DOMAIN ANALYSIS; WINGS;

NONLINEAR AEROELASTIC ANALYSIS;

FIGHTER AIRCRAFT;

EID: 0036651053     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/2.2984     Document Type: Article

References (20)

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6. Analysis of limit cycle flutter of an airfoil in incompressible flow
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8. Non-linear behavior of a typical airfoil section with control surface freeplay: A numerical and experimental study
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13. Accelerated convergence for vibration modes using the substructure coupling method and fictitious coupling masses
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