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TECHNICAL PAPERS

Buckling of Laminated Composite Rectangular Plates Under Transient Thermal Loading

[+] Author and Article Information
K. K. Shukla

Applied Mechanics Department, M.N.R. Engineering College, Allahabad 211004, India

Y. Nath

Applied Mechanics Department, I.T.T., Delhi 110016, India

J. Appl. Mech 69(5), 684-692 (Aug 16, 2002) (9 pages) doi:10.1115/1.1485755 History: Received February 01, 2001; Revised November 15, 2001; Online August 16, 2002
Copyright © 2002 by ASME
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References

Figures

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Geometry of laminated plate
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Central displacement response for antisymmetric angle-ply [45/-45/45/-45] square SSSS plate (a/h=20, Material B) under in-plane uniform thermal loading
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Central displacement response for unsymmetric angle-ply [0/15/30/45] square SSSS plate (a/h=20, Material B) under in-plane uniform thermal loading
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Central displacement response for symmetric cross-ply [0/90/90/0] square CSCS plate (a/h=20, Material A) under in-plane uniform thermal loading
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Central displacement response for antisymmetric cross-ply [0/90/0/90] square CCSS plate (a/h=20, Material A) under in-plane uniform thermal loading
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Central displacement response for antisymmetric cross-ply [0/90/0/90] square CSSS plate (a/h=20, Material A) under in-plane uniform thermal loading
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Dynamic thermal post-buckling response of laminated composite plates (a/h=20) under in-plane uniform thermal loading

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