Buckling of Angle-Ply Laminated Circular Cylindrical Shells

[+] Author and Article Information
Y. Hirano

Department of Mechanical Engineering, Aeronautical Engineering and Mechanics, Rensselaer Polytechnic Institute, Troy, New York

J. Appl. Mech 46(1), 233-234 (Mar 01, 1979) (2 pages) doi:10.1115/1.3424514 History: Received August 01, 1978; Revised November 01, 1978; Online July 12, 2010


This Note presents closed-farm solutions for axisymmetrical and axially unsymmetrical buckling of angle-ply laminated circular cylindrical shells under axial compression. The axisymmetrical and axially unsymmetrical buckling stress are found to be different from each other, and the best lamination angles which give the highest buckling stress are obtained.

Copyright © 1979 by ASME
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