Interlaminar Stresses in Symmetric Composite Laminates-Reference-Cited by-同舟云学术

Interlaminar Stresses in Symmetric Composite Laminates

Published:1978-12 Issue:4 Volume:12 Page:390-402
ISSN:0021-9983
Container-title:Journal of Composite Materials
language:en
Short-container-title:Journal of Composite Materials

Author:

Wang James T.S.¹,Dickson John N.²

Affiliation:

1. School of Engineering Science and Mechanics Georgia Institute of Technology Atlanta, Georgia 30332

2. Advanced Structures Department Lockheed-Georgia Company Marietta, Georgia 30063

Abstract

Interlaminar stresses and displacements of each layer satisfying geo metrical boundary conditions are represented in series of Legendre poly nomials. The extended Galerkin procedure is used for each layer, and the final solutions are obtained by requiring the satisfaction of continuity conditions at each interface and the stress boundary conditions at exterior planes. A computer program has been prepared, and numerical results are presented and compared with existing data.

Publisher

SAGE Publications

Subject

Materials Chemistry,Mechanical Engineering,Mechanics of Materials,Ceramics and Composites

Link

http://journals.sagepub.com/doi/pdf/10.1177/002199837801200404

Reference10 articles.

1. Some observations on the interlaminar strength of composite laminates

2. Approximate Three-Dimensional Solutions for Symmetric Laminates Under Inplane Loading *

3. Interlaminar Stresses in Composite Laminates Under Uniform Axial Extension

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