Application of aeroelastic modes on nonlinear supersonic panel flutter at elevated temperatures

Computers and Structures

Volumn 84, Issue 24-25, 2006, Pages 1619-1628

  Guo, Xinyun ^a   Mei, Chuh ^b  

^a SOUTHERN NEW HAMPSHIRE UNIVERSITY   (United States)

^b Old Dominion University   (United States)

Author keywords

Aeroelasticity; Composite plates; Finite element analysis; Nonlinear analysis; Panel flutter; Supersonic speeds

Indexed keywords

COMPOSITE MATERIALS; FINITE ELEMENT METHOD; FLUTTER (AERODYNAMICS); MODAL ANALYSIS; NONLINEAR SYSTEMS; OSCILLATIONS; STRUCTURAL PANELS; SUPERSONIC AERODYNAMICS;

COMPOSITE PLATES; NONLINEAR ANALYSIS; PANEL FLUTTER; SUPERSONIC SPEEDS;

AERODYNAMICS;

EID: 33746864521     PISSN: 00457949     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.compstruc.2006.01.041     Document Type: Article

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