An efficient iterative model reduction method for aeroviscoelastic panel flutter analysis in the supersonic regime-Reference-Cited by-同舟云学术

An efficient iterative model reduction method for aeroviscoelastic panel flutter analysis in the supersonic regime

Published:2018-05 Issue: Volume:104 Page:575-588
ISSN:0888-3270
Container-title:Mechanical Systems and Signal Processing
language:en
Short-container-title:Mechanical Systems and Signal Processing

Author:

Cunha-Filho A.G.,Briend Y.P.J.,de Lima A.M.G.,Donadon M.V.

Funder

Brazilian Research Council

Publisher

Elsevier BV

Subject

Computer Science Applications,Mechanical Engineering,Aerospace Engineering,Civil and Structural Engineering,Signal Processing,Control and Systems Engineering

Reference29 articles.

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2. Flutter of rectangular composite plates with variable fiber spacing;Kuo;Compos. Struct.,2011

3. A parametric study on supersonic flutter behavior of laminated composite skew flat panels;Singha;Compos. Struct.,2005

4. Implications of cubic physical/aerodynamic non-linearities on the character of the flutter instability boundary;Librescu;Int. J. Non-linear Mech.,2003

5. Active aeroelastic control with time delay for targeted flutter modes;Singh;Aerosp. Sci. Technol.,2015

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