Proper orthogonal decomposition method for analysis of nonlinear panel flutter with thermal effects in supersonic flow-Reference-Cited by-同舟云学术

Proper orthogonal decomposition method for analysis of nonlinear panel flutter with thermal effects in supersonic flow

Published:2015-02 Issue: Volume:337 Page:263-283
ISSN:0022-460X
Container-title:Journal of Sound and Vibration
language:en
Short-container-title:Journal of Sound and Vibration

Author:

Xie Dan^ORCID,Xu Min,Dai Honghua,Dowell Earl H.

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,Acoustics and Ultrasonics,Condensed Matter Physics

Reference33 articles.

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3. A finite-element approach for nonlinear panel flutter;Mei;AIAA Journal,1977

4. Aeroelastic stability analysis of heated panel with aerodynamic loading on both surfaces;Zhou;Science China: Technological Sciences,2012

5. A simple proper orthogonal decomposition method for von Karman plate undergoing supersonic flow;Xie;Computer Modeling in Engineering and Sciences,2013

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