Non-linear transient response of fluttering stiffened composite plates subject to thermal load

Journal of Sound and Vibration

Volumn 245, Issue 4, 2001, Pages 715-736

  Oh, I K ^a   Lee, I ^a   Lee, D M ^b  

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

^b Agency for Defence Development   (South Korea)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC LOADS; BENDING (DEFORMATION); CHAOS THEORY; COMPOSITE MATERIALS; FINITE ELEMENT METHOD; FLUTTER (AERODYNAMICS); THERMAL LOAD; TIME DOMAIN ANALYSIS;

TRANSIENT RESPONSE;

PLATES (STRUCTURAL COMPONENTS);

EID: 0035939963     PISSN: 0022460X     EISSN: None     Source Type: Journal    
DOI: 10.1006/jsvi.2001.3576     Document Type: Article

References (12)

1. Panel flutter: A review of the aeroelastic stability of plates and shells
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3. Effects of inplane load on nonlinear panel flutter by incremental harmonic balance method
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5. Finite element time domain-modal formulation for nonlinear flutter of composite panels
6. Nonlinear flutter of orthotropic composite panel under aerodynamic heating
7. On the understanding of snap-through phenomenon in aerothermoelasticity of panels
8. Flutter analysis of stiffened laminated composite plates and shells in supersonic flow
9. Supersonic flutter analysis of stiffened isotropic and anisotropic panels
10. Supersonic flutter analysis of stiffened laminated plates subject to thermal load
11. Vibration analysis of anisotropic plates with eccentric stiffeners
12. Nonlinear transient responses of initially stressed composite plates