郝鹏

个人信息Personal Information

教授

博士生导师

硕士生导师

主要任职:Professor

其他任职:工程力学系主任

性别:男

毕业院校:大连理工大学

学位:博士

所在单位:力学与航空航天学院

学科:固体力学. 航空航天力学与工程. 计算力学. 工程力学

联系方式:haopeng@dlut.edu.cn

电子邮箱:haopeng@dlut.edu.cn

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A high-fidelity approximate model for determining lower-bound buckling loads for stiffened shells

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论文类型:期刊论文

发表时间:2018-09-01

发表刊物:INTERNATIONAL JOURNAL OF SOLIDS AND STRUCTURES

收录刊物:SCIE、EI

卷号:148

期号:,SI

页面范围:14-23

ISSN号:0020-7683

关键字:Shell buckling; Imperfection sensitivity; Modal Assurance Criterion; Representative Volume Element method; Optimization

摘要:The Worst Multiple Perturbation Load Approach (WMPLA) has been validated by full-scale tests to be an effective and credible determination method for the lower-bound buckling load of stiffened shells. In spite of its high prediction accuracy and robustness, the large computational time is a burden because this method is based on the large-scale optimization of detailed finite element (FE) models. Therefore, a high-fidelity approximate modeling strategy is proposed in this paper, to improve the efficiency of WM-PLA and then promote its application for the preliminary design stage of stiffened shells. In the first step, an initial approximate model is established by means of the Representative Volume Element (RVE) equivalent method. In the second step, a modified equivalent model is generated after optimizing the effective stiffness coefficients of the initial equivalent model. In the optimization process, the objective is minimizing the relative error in buckling load between a detailed FE model and the modified approximate model. The constraint condition is controlled by the Modal Assurance Criterion (MAC) coefficients for buckling mode. In particular, the global and local deformation features are simultaneously considered in the MAC coefficients. After the establishment of the high-fidelity approximate model, it is then integrated into WMPLA. By optimization of the positions and amplitudes of the multiple perturbation loads, the minimum buckling load is obtained as the lower-bound value. By comparison against known methods, the lower-bound buckling load predicted by the proposed strategy is quite close to the test result, succeeding in providing a safe design load prediction. The proposed strategy reduces the computational time sharply by 94% compared to the WMPLA based on detailed FE models, indicating high efficiency. Additionally, an illustrative example is shown to highlight the importance of the prediction accuracy of buckling mode on the fidelity of approximate models for WMPLA. Finally, it is concluded that the proposed strategy is a potential and efficient approach to predict lower-bound buckling loads of stiffened shells. (C) 2017 Elsevier Ltd. All rights reserved.