Buckling and vibration of stiffened plates subjected to partial edge loading |
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| Authors: | A K L Srivastava P K Datta A H Sheikh |
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| Affiliation: | a Department of Aerospace Engineering, Indian Institute of Technology, Kharagpur 721302, India;b Department of Ocean Engineering and Naval Architecture, Indian Institute of Technology, Kharagpur 721302, India |
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| Abstract: | The buckling and vibration characteristics of stiffened plates subjected to in-plane partial and concentrated edge loadings are studied using finite element method. The initial stresses are obtained considering the pre-buckling conditions. Buckling loads and vibration frequencies are determined for different plate aspect ratios, edge conditions and different partial non-uniform edge loading cases. The non-uniform loading may also be caused due to the supports on the edges. The analysis presented determines the stresses all over the region for different kinds of loading and edge conditions. In the structural modelling, the plate and the stiffeners are treated as separate elements where the compatibility between these two types of elements is maintained. The vibration characteristics are discussed and the results are compared with those available in the literature. Buckling results show that the stiffened plate is less susceptible to buckling for position of loading near the supported edges and near the position of stiffeners as well. |
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| Keywords: | FEM Partial edge loadings Buckling load Vibration frequency Stiffener |
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