TECHNICAL NOTES
Mar 1, 1989
Cylindrical Buckling Load of Laminated Columns
Publication: Journal of Engineering Mechanics
Volume 115, Issue 3
Abstract
The cylindrical buckling load of a composite laminated column is derived from plate theory. The effect of lamina orientation is taken into account by treating the stiffness parameter as a matrix product rather than as a single value drawn from the definition of the elastic coefficients. This refined stiffness parameter leads to significant improvement of the buckling load, depending on the stacking combination and orientation.
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References
1.
Calcote, L. R. (1969). The analysis of laminated composite structures. Van Nostrand Reinhold, New York, N.Y.
2.
Sheinman, I., Shaw, D., and Simitses, G. J. (1983). “Nonlinear analysis of axially loaded laminated cylindrical shells.” Comput. Struct. 16(1–4), 131–137.
3.
Vinson, J. R., and Sierakowski, R. L. (1986). The behavior of structures composed of composite materials. Martinus Nijhoff, Dordrecht, Netherlands.
Information & Authors
Information
Published In
Journal of Engineering Mechanics
Volume 115 • Issue 3 • March 1989
Pages: 659 - 661
Copyright
Copyright © 1989 ASCE.
History
Published online: Mar 1, 1989
Published in print: Mar 1989
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Authors
Affiliations
Izhak Sheinman
Assoc. Prof., Dept. of Civ. Engrg., TECHNION—Israel Inst. of Tech., Technion City, Haifa 32 000, Israel
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Terms of Use: ASCE Library Cards are for individual, personal use only. Reselling, republishing, or forwarding the materials to libraries or reading rooms is prohibited.
Terms of Use: ASCE Library Cards are for individual, personal use only. Reselling, republishing, or forwarding the materials to libraries or reading rooms is prohibited.