Interaction formulae for buckling and failure of orthotropic plates under combined axial compression/tension and shear |
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Authors: | Binwen WANG Xiangming CHEN Xiasheng SUN Puhui CHEN Zhe WANG Ya'nan CHAI |
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Institution: | 1. Aeronautics Science and Technology Key Laboratory of Full Scale Aircraft Structure and Fatigue, Aircraft Strength Research Institute of China, Xi’an 710065, China;2. Chinese Aeronautical Establishment, Beijing 100029, China;3. State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China |
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Abstract: | An interaction function was constructed based on the axial compression/tension and shear loads of orthotropic plates. The coefficients of the polynomial function were determined by uniaxial test results. Buckling interaction and failure interaction formulae under combined axial tension/compression and shear loads were established. Based on the uniaxial load test results of orthotropic plates, the buckling load and bearing capacity under any proportion of the combined loads could be predicted by using the proposed interaction formulae. The buckling interaction curves and failure envelopes predicted by the proposed interaction formulae were in excellent agreement with the test results. |
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Keywords: | Buckling Combined loads Failure Interaction formulae Orthotropic plate |
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