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[Abstract]:Based on the Euler beam and elastic thin plate theory, this paper analyzes six failure modes and the corresponding nominal stresses of the plate model of the second-order fold structure under shear or compression loads. By comparing the nominal stress values, the failure mode types are controlled, and the performance optimization of minimum weight and minimum deflection is carried out in combination with the multi-objective optimization algorithm. In this paper, two optimization models are established: one is to control the type of failure mode that occurs for the first time, and the other is to classify the failure mode according to the loss size and occur according to the grade sequence. On this basis, the performance indexes of typical design points in Pareto frontier diagram of two optimization models are discussed, and finally, the failure mode types are verified by finite element analysis. The results show that the structural design obtained by the two optimization models is consistent with the type of control occurrence, and the comprehensive performance is greatly improved. The second model takes into account the difference of stress value and prevents the structure from suddenly failing as a whole, which is safer.
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[Abstract]:Based on the Euler beam and elastic thin plate theory, this paper analyzes six failure modes and the corresponding nominal stresses of the plate model of the second-order fold structure under shear or compression loads. By comparing the nominal stress values, the failure mode types are controlled, and the performance optimization of minimum weight and minimum deflection is carried out in combination with the multi-objective optimization algorithm. In this paper, two optimization models are established: one is to control the type of failure mode that occurs for the first time, and the other is to classify the failure mode according to the loss size and occur according to the grade sequence. On this basis, the performance indexes of typical design points in Pareto frontier diagram of two optimization models are discussed, and finally, the failure mode types are verified by finite element analysis. The results show that the structural design obtained by the two optimization models is consistent with the type of control occurrence, and the comprehensive performance is greatly improved. The second model takes into account the difference of stress value and prevents the structure from suddenly failing as a whole, which is safer.
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