Boundary layer theory for the buckling and postbuckling of an anisotropic laminated cylindrical shell. Part I: Prediction under axial compression

Author:

Shen Hui-Shen

Publisher

Elsevier BV

Subject

Civil and Structural Engineering,Ceramics and Composites

Reference35 articles.

1. Buckling of laminated anisotropic imperfect circular cylinders under axial compression;Tennyson;J Spacecraft,1973

2. Kobayashi S, Koyama K, Seko H. Compressive buckling of graphite–epoxy composite circular cylindrical shells. In: Proceedings of the 23rd AIAA/ASME/ASCE/AHS structures, structural dynamics, and materials conference, New Orleans, May 1982.

3. Buckling tests with axially compressed unstiffened cylindrical shells made from CFRP;Geier,1991

4. Experimental buckling of thin composite cylinders in compression;Bisagni;AIAA J,1999

5. Compression tests on anti-symmetric two-ply GFRP cylinders;Chryssanthopoulos;Composites Part B,1999

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