Buckling of Laminated Cylindrical Panels under Uniaxial Compression

Author

K. Chandrashekhara, Missouri University of Science and TechnologyFollow

Abstract

Buckling characteristics of anisotropic laminated cylindrical panels are presented using an isoparametric nine-noded rectangular element. Kinematic relations, extended to include the first-order shear deformation theory, are utilized in the formulation. Numerical results are presented for laminated cylindrical panels under uniaxial compression loading to illustrate the influence of panel sizes, orientation of layers, material properties, and boundary conditions on the buckling loads. Results for plates are also presented as special cases and are compared with the available solutions.

Recommended Citation

K. Chandrashekhara, "Buckling of Laminated Cylindrical Panels under Uniaxial Compression," Journal of Energy Resources Technology, American Society of Mechanical Engineers (ASME), Jan 1991.

The definitive version is available at https://doi.org/10.1115/1.2905908

Department(s)

Mechanical and Aerospace Engineering

Keywords and Phrases

Buckling; Compression; Shear Deformation; Stress; Materials Properties; Plates (Structures); Boundary-Value Problems

International Standard Serial Number (ISSN)

0195-0738

Document Type

Article - Journal

Document Version

Citation

File Type

text

Language(s)

English

Rights

© 1991 American Society of Mechanical Engineers (ASME), All rights reserved.

Publication Date

01 Jan 1991