TECHNICAL PAPERS
Mar 8, 2010

Closed-Form Solutions for Buckling of Long Anisotropic Plates with Various Boundary Conditions under Axial Compression

Publication: Journal of Engineering Mechanics
Volume 136, Issue 9

Abstract

Closed-form solutions for buckling of long plates with flexural/twist anisotropy with the short edges simply supported and with the longitudinal edges simply supported, clamped, or elastically restrained in rotation under axial compression are presented. An energy method (Rayleigh–Ritz) is employed to obtain the critical buckling loads. The critical buckling loads are expressed in terms of minimum nondimensional buckling coefficients and stiffness parameters. The new closed-form solutions show an excellent agreement when compared to existing solutions and finite-element analysis. Due to their simplicity and accuracy, the new closed-form solutions can be confidently used as an alternative to computationally expensive structural analysis to assess buckling in the preliminary design phase of composite structures.

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Acknowledgments

The writers thank the European Commission for the Marie-Curie Excellence Grant No. UNSPECIFIEDMEXT-CT-2003-002690.

References

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Information & Authors

Information

Published In

Go to Journal of Engineering Mechanics
Journal of Engineering Mechanics
Volume 136Issue 9September 2010
Pages: 1105 - 1114

History

Received: Jul 31, 2008
Accepted: Feb 24, 2010
Published online: Mar 8, 2010
Published in print: Sep 2010

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Authors

Affiliations

J. Enrique Herencia [email protected]
Visiting Research Fellow, Dept. of Aerospace Engineering, Univ. of Bristol, Queen’s Building, Bristol BS8 1TR, U.K. (corresponding author). E-mail: [email protected]
Paul M. Weaver
Professor, Dept. of Aerospace Engineering, Univ. of Bristol, Queen’s Building, Bristol BS8 1TR, U.K.
Michael I. Friswell
Professor, School of Engineering, Swansea Univ., Singleton Park, Swansea SA2 8PP, U.K.

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