Title

Buckling of Compression Loaded Laminated Composite Cylindrical Panels

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 through the thickness of the laminate, are utilized in the formulation. Numerical results are presented for laminated cylindrical panels under uniaxial and biaxial compression loadings 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.

Meeting Name

Composite Material technology 1989

Department(s)

Mechanical and Aerospace Engineering

Keywords and Phrases

Cylinders-Composite; Kinematics; Laminated Products-Deformation; Stresses-Shear

Document Type

Article - Conference proceedings

Document Version

Citation

File Type

text

Language(s)

English

Rights

© 1989 American Society of Mechanical Engineers (ASME), Petroleum Division, All rights reserved.

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