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Exact eigensolutions for flutter of two-dimensional symmetric cross-ply composite laminates at high supersonic speeds

  • Published:2018-01 Issue: Volume:183 Page:358-370
  • ISSN:0263-8223
  • Container-title:Composite Structures
  • language:en
  • Short-container-title:Composite Structures

Author:

Sun Qiaozhen,Xing Yufeng

Funder

National Natural Science Foundation of China

Research Fund for the Doctoral Program of Higher Education of China

Publisher

Elsevier BV

Subject

Civil and Structural Engineering,Ceramics and Composites

Reference63 articles.

1. Historical development of aircraft flutter;Garrick;J Aircr,1981

2. Some recent developments in flutter of flat panels;Bohon;J Aircr,1964

3. A summary of the theories and experiments on panel flutter;Fung,1960

4. Flutter research on skin panels. NASA TN D-451;Kordes,1960

5. Bohon HL. Panel flutter tests on full-scale X-15 lower vertical stabilizer at Mach number of 3.0. NASA TN D-1385; 1962.

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