Panel flutter characteristics of sandwich plates with CNT reinforced facesheets using an accurate higher-order theory

Author:

Sankar A.,Natarajan S.,Haboussi M.,Ramajeyathilagam K.,Ganapathi M.

Funder

School of Civil and Environmental Engineering, The University of New South Wales, Sydney

Publisher

Elsevier BV

Subject

Mechanical Engineering

Reference31 articles.

1. A new theory for accurate thermal/mechanical flexural analysis of symmetrically laminated plates;Ali;Composite Structures,1999

2. Eshelby–Mori–Tanaka approach for vibration behavior of continuously graded carbon nanotube-reinforced cylindrical panels;Aragh;Composites Part B: Engineering,2012

3. Buckling analysis of laminated composite rectangular plates reinforced by SWCNTs using analytical and finite element methods;Arani;Journal of Mechanical Science and Technology,2011

4. Assess the accuracy of the variational asymptotic plate and shell analysis using the generalized unified formulation;Demasi;Mechanics of Advanced Materials and Structures,2013

5. Dixon, S.C., Hudson, M.L., 1970. Flutter, Vibration and Buckling of Truncated Orthotropic Conical Shells with Generalized Elastic Edge Restraints. NASA TN D-5759.

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