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TECHNICAL PAPERS

Buckling Optimization of Composite Axisymmetric Cylindrical Shells Under Uncertain Loading Combinations

[+] Author and Article Information
A. R. de Faria, J. S. Hansen

Institute for Aerospace Studies, UTIAS, 4925 Dufferin Street, Toronto, Ontario M3H 5T6, Canada

J. Appl. Mech 68(4), 632-639 (Feb 07, 2000) (8 pages) doi:10.1115/1.1311962 History: Received September 29, 1999; Revised February 07, 2000
Copyright © 2001 by ASME
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References

Figures

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Cylinder subjected to mechanical loads and boundary conditions
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Geometric interpretation
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Effect of uncertainty degree on the optimal critical load
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(a) Load space—case 1a; (b) load space—case 2b; (c) load space—case 3c (d) load space—case 4
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(a) Comparative performance—axial compression; (b) comparative performance—lateral pressure; (c) comparative performance—torsion

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