Through-the-thickness stress distributions near edges of composite laminates using stress recovery scheme and third order shear and normal deformable theory-Reference-Cited by-同舟云学术

Through-the-thickness stress distributions near edges of composite laminates using stress recovery scheme and third order shear and normal deformable theory

Published:2015-11 Issue: Volume:131 Page:397-413
ISSN:0263-8223
Container-title:Composite Structures
language:en
Short-container-title:Composite Structures

Author:

Shah P.H.,Batra R.C.

Funder

Office of Naval Research

Publisher

Elsevier BV

Subject

Civil and Structural Engineering,Ceramics and Composites

Reference57 articles.

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5. The theory of shells and plates;Naghdi,1973

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