Compression Buckling Response of Tailored Rectangular Composite Plates-Reference-Cited by-同舟云学术

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Compression Buckling Response of Tailored Rectangular Composite Plates

Published:1993-03 Issue:3 Volume:31 Page:590-596
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Biggers Sherrill B.¹,Srinivasan Sundar¹

Affiliation:

1. Clemson University, Clemson, South Carolina 29634

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.61543

Reference4 articles.

1. ^ulson, P. S., The Stability of Flat Plates, American Elsevier Publishing, New York, 1969, pp.130-132.

2. 2ABAQUS Theory and User's Manuals, Version 4.8, Hibbitt, Karlsson, and Sorensen Inc.,Pawtucket, RI, 1989.

3. 4Tsai, S. W., and Hahn, H. T., Introduction to Composite Materials, Technomic Publishers, Westport, CT, 1980, pp.394-401.

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