The effect of flexural/twist anisotropy on compression buckling of quasi-isotropic laminated cylindrical shells-Reference-Cited by-同舟云学术

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The effect of flexural/twist anisotropy on compression buckling of quasi-isotropic laminated cylindrical shells

Published:2002-02 Issue:2 Volume:55 Page:195-204
ISSN:0263-8223
Container-title:Composite Structures
language:en
Short-container-title:Composite Structures

Author:

Weaver P.M.,Driesen J.R.,Roberts P.

Publisher

Elsevier BV

Subject

Civil and Structural Engineering,Ceramics and Composites

Reference32 articles.

1. Design of laminated composite cylindrical shells under axial compression;Weaver;Composites B,2000

2. Weaver PM. Computer aided laminate selection using a graphical method. ICCM12, July 5–9, Paris, 1999

3. Mechanics of composite materials;Jones,1999

4. Lay-up optimisation against buckling of shear panels;Grenestedt;Struct. Optim.,1991

5. Mechanics of composite materials;Vasiliev,1993

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