Bounds on Flexural Properties and Buckling Response for Symmetrically Laminated Composite Plates-Reference-Cited by-同舟云学术

Bounds on Flexural Properties and Buckling Response for Symmetrically Laminated Composite Plates

Published:2007-11 Issue:11 Volume:133 Page:1178-1191
ISSN:0733-9399
Container-title:Journal of Engineering Mechanics
language:en
Short-container-title:J. Eng. Mech.

Author:

Weaver Paul M.¹²,Nemeth Michael P.¹²

Affiliation:

1. Dept. of Aerospace Engineering, Queen’s Building, Univ. of Bristol, Bristol BS8 1TR, U.K. (corresponding author). E-mail: paul.weaver@bristol.ac.uk

2. Structural Mechanics and Concepts Branch, NASA Langley Research Center, Hampton, VA.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Mechanics of Materials

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%290733-9399%282007%29133%3A11%281178%29

Reference31 articles.

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4. Buckling of anisotropic composite plates;Chamis C. C.;J. Struct. Div.,1969

5. Fukunaga H. and Hirano Y. (1982). “Stability optimization of laminated composite plates under in-plane loads.” Proc. 4th Int. Conf. on Composite Materials Vol. 1 Tokyo 565–572.

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