Analysis of a Long Thick Orthotropic Circular Cylindrical Shell Panel

Abstract

An exact three-dimensional elasticity solution has been obtained for an infinitely long, thick transversely isotropic circular cylindrical shell panel, simply supported along the longitudinal edges and subjected to a radial patch load. Using a set of three displacement functions, the boundary value problem is reduced to Bessel's differential equation. Numerical results are presented for different thickness to mean radius ratios and semicentral angles of the shell panel. Classical and first-order shear deformation orthotropic shell theories have been examined in comparison with the present elasticity solution.

Department(s)

Mechanical and Aerospace Engineering

International Standard Serial Number (ISSN)

0733-9399

Document Type

Article - Journal

Document Version

Citation

File Type

text

Language(s)

English

Rights

© 1996 American Society of Civil Engineers (ASCE), All rights reserved.

Publication Date

01 Jan 1996

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