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作 者:Wensheng Wang Haojie Wei Zhonghua Hou Qun Mei Yifan Li
机构地区:[1]Department of Engineering Mechanics, Henan University of Science and Technology
出 处:《Journal of Harbin Institute of Technology(New Series)》2019年第3期68-78,共11页哈尔滨工业大学学报(英文版)
基 金:Sponsored by the National Natural Science Foundation of China(Grant No.11402077)
摘 要:A finite element model updating technique for complicated beam-type structures is presented in this study.Firstly, a complicated beam-type structure is reduced to a reduced super beam model with a much smaller degree of freedom by using the reduced super beam method, which is based on the classic plane cross-section assumption and displacement interpolation function of beam theory.Then based on the reduced super beam, the analysis of eigensolutions and eigensensitivities from the reduced eigenequation are processed for model updating, which will greatly reduce the computational effort when compared to the traditional model updating methods performed on the global model.Optimization techniques are adopted for updating the difference of modal dynamic properties, resulting in optimal values of the structural parameters.Finally, a complicated stiffened cylindrical shell model and a practical missile structure, served as the illustrative examples, are employed for model updating application, which demonstrate that the reduced super beam-based method is both effective and highly efficient.A finite element model updating technique for complicated beam-type structures is presented in this study. Firstly, a complicated beam-type structure is reduced to a reduced super beam model with a much smaller degree of freedom by using the reduced super beam method, which is based on the classic plane cross-section assumption and displacement interpolation function of beam theory. Then based on the reduced super beam, the analysis of eigensolutions and eigensensitivities from the reduced eigenequation are processed for model updating, which will greatly reduce the computational effort when compared to the traditional model updating methods performed on the global model. Optimization techniques are adopted for updating the difference of modal dynamic properties, resulting in optimal values of the structural parameters. Finally, a complicated stiffened cylindrical shell model and a practical missile structure, served as the illustrative examples, are employed for model updating application, which demonstrate that the reduced super beam-based method is both effective and highly efficient.
关 键 词:REDUCED super BEAM method model updating COMPLICATED beam-type STRUCTURES EIGENSOLUTION eigensensitivity
分 类 号:V214[航空宇航科学与技术—航空宇航推进理论与工程] V414
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