Title

Static Analysis of Thick Laminated Circular Cylindrical Shells

Abstract

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.

Department(s)

Mechanical and Aerospace Engineering

Keywords and Phrases

Circular Cylindrical Shells; Laminates; Stress; Shear Deformation; Shells; Elasticity

Document Type

Article - Journal

Document Version

Citation

File Type

text

Language(s)

English

Rights

© 1993 American Society of Mechanical Engineers (ASME), All rights reserved.


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