Citation
Toda, Susumu (1975) The Effects of Elliptic and Rectangular Cutouts on the Buckling of Cylindrical Shells Loaded by Axial Compression. Engineer's thesis, California Institute of Technology. doi:10.7907/473V-C743. https://resolver.caltech.edu/CaltechETD:etd-12042006-090542
Abstract
The results of experimental investigations of the effect of elliptic cutouts on the buckling of thin cylindrical shells under axial compression are presented. The experiments were performed on Mylar shells with a radius to thickness ratio of 400 and with two diametrically opposed circular, elliptic or rectangular holes. The results show that, for a given shell geometry, the area of a cutout determined the shell buckling behavior, but that the configuration of the cutout had little influence on the buckling loads. A simplified analytical study based on Van Dyke's stress analysis and a strictly empirical design formula which gives a lower bound for the existing experimental data are also presented.
Item Type: | Thesis (Engineer's thesis) |
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Subject Keywords: | (Aeronautical Engineering) |
Degree Grantor: | California Institute of Technology |
Division: | Engineering and Applied Science |
Major Option: | Aeronautics |
Thesis Availability: | Public (worldwide access) |
Research Advisor(s): |
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Group: | GALCIT |
Thesis Committee: |
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Defense Date: | 13 August 1974 |
Record Number: | CaltechETD:etd-12042006-090542 |
Persistent URL: | https://resolver.caltech.edu/CaltechETD:etd-12042006-090542 |
DOI: | 10.7907/473V-C743 |
Default Usage Policy: | No commercial reproduction, distribution, display or performance rights in this work are provided. |
ID Code: | 4776 |
Collection: | CaltechTHESIS |
Deposited By: | Imported from ETD-db |
Deposited On: | 20 Dec 2006 |
Last Modified: | 31 Jul 2024 22:54 |
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