Buckling optimization of laminated cylindrical panels subjected to axial compressive load-Reference-Cited by-同舟云学术

Buckling optimization of laminated cylindrical panels subjected to axial compressive load

Published:2007-12 Issue:3 Volume:81 Page:374-385
ISSN:0263-8223
Container-title:Composite Structures
language:en
Short-container-title:Composite Structures

Author:

Hu Hsuan-Teh,Yang Jiing-Sen

Publisher

Elsevier BV

Subject

Civil and Structural Engineering,Ceramics and Composites

Reference24 articles.

1. Buckling analysis of laminated composite plates;Crouzet-Pascal;Fibre Sci Technol,1978

2. Optimum design of laminated plates under axial compression;Hirano;AIAA J,1979

3. Leissa AW. Buckling of laminated composite plates and shell panels. AFWAL-TR-85-3069, Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Wright-Patterson Air Force Base, OH; 1985.

4. Optimal fibre orientation for simply-supported angle-ply plates under biaxial compression;Muc;Compos Struct,1988

5. Buckling optimization of symmetrically laminated rectangular plates with various geometry and end conditions;Hu;Compos Sci Technol,1995

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