Static Analysis of Thick Laminated Circular Cylindrical Shells

[+] Author and Article Information
K. Chandrashekhara, B. S. Kumar

Department of Civil Engineering, Indian Institute of Science, Bangalore, India

J. Pressure Vessel Technol 115(2), 193-200 (May 01, 1993) (8 pages) doi:10.1115/1.2929515 History: Received July 29, 1991; Revised December 22, 1992; Online June 17, 2008


An approximate solution for a thick laminated simply supported circular cylindrical shell of revolution and shell panel subjected to asymmetric load has been obtained using elasticity approach. The results obtained from this analysis have been compared with the exact solution. Numerical results have been presented for 3-ply hybrid laminates and (0/90/0) laminates subjected to patch loads. The results have also been compared with some available classical and shear deformation theories to assess the accuracy of these theories.

Copyright © 1993 by The American Society of Mechanical Engineers
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