Elastic large deflection analysis of unstiffened and stiffened plates under linearly-varying edge compressive loading
Call Number: AIT Thesis no.1036 Material type:
SeriesSeries: Asian Institute of Technology. Thesis ; no. 1036Publication details: Bangkok : Asian Institute of Technology, 1977Description: 34 pSubject(s): Online resources: Dissertation note: Thesis (M.Eng.) - Asian Institute of Technology, 1977 Summary: The elastic post-buckling behavior of stiffened and unstiffened rectangular plates under linearly varying edge compression is presented. Theoretical analysis of s imply supported plates with two different unloaded edge conditions is considered. The effects of initial imperfections are allowed for in the analysis. The theoretical investigation begins with the Marguerre 's compatibility equation and proceeds to obtain a solution by the energy method. In this paper, the collapse criterion is so specified that the mean membrane stress along the unloaded edge reaches the yield stress of the plate material. Numerical results are presented graphically and compared with some available test results.
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40-Archives
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Asian Institute of Technology Library Archives | AIT Thesis no.1036 (Browse shelf(Opens below)) | Available | 30050160088901 |
A thesis submitted in partial fulfillment of the requirements for the degree of Master of Engineering of the Asian Institute of Technology, Bangkok, Thailand.
Thesis (M.Eng.) - Asian Institute of Technology, 1977
The elastic post-buckling behavior of stiffened and unstiffened rectangular plates under linearly varying edge compression is presented. Theoretical analysis of s imply supported plates with two different unloaded edge conditions is considered. The effects of initial imperfections are allowed for in the analysis. The theoretical investigation begins with the Marguerre 's compatibility equation and proceeds to obtain a solution by the energy method. In this paper, the collapse criterion is so specified that the mean membrane stress along the unloaded edge reaches the yield stress of the plate material. Numerical results are presented graphically and compared with some available test results.
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