Research Article
Jul 1975
Stability of Hyperboloidal Shells
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VIEW THE REPLYPublication: Journal of the Structural Division
Volume 101, Issue 7
Abstract
An analytical and experimental investigation was carried out to determine the buckling loads of hyperboloidal shells with different geometries subjected to the axisymmetric loadings of external pressure and axial compression. Sander's thin shell equations were used in conjunction with the finite element method to determine the bifurcation buckling load of the shell. The experimental program yielded data on the instability behavior of hyperboloidal shells subjected to combined loadings. Molded PVC specimens were used in the experiments. Shell specimens were: (1) Clamped on both ends; and (20 clamped on one end and free on the other end. The experimental data were found to be in good agreement with the analysis for all types of loading conditions.
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Published In
Journal of the Structural Division
Volume 101 • Issue 7 • July 1975
Pages: 1585 - 1602
Copyright
© 1975 American Society of Civil Engineers.
History
Published in print: Jul 1975
Published online: Feb 1, 2021
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Authors
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Daniel R. Veronda
Staff Engr., Hughes Aircraft Co., Fullerton, Calif.
Victor I. Weingarten, M.ASCE
Prof. of Civ. Engrg., Univ. of Southern California, Los Angeles, Calif.
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ASCE Library Cards let you download journal articles, proceedings papers, and available book chapters across the entire ASCE Library platform. ASCE Library Cards remain active for 24 months or until all downloads are used. Note: This content will be debited as one download at time of checkout.
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.