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Error localization of finite element updating model based on element strain energy

机译:基于元应变能量的有限元更新模型的误差定位

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An error localization indicator based on modal strain energy changes is proposed and used for selecting design parameters to be updated in model updating process. Taking an aero-engine combustor casing structure as an example, the 'supermodel' of combustor casing was established and validated with the test data and the reduced model (also called the design model) was built with the simplification of modelling. By comparing the modal strain energy changes between 'supermodel' and design model of combustor casing, the error locations of the reduced combustor casing modelling was highlighted by the error localization indicator. Then, the updating parameters of the design model were selected as the areas with significant variations of modal strain energy changes based on the error localization indicator. Defining the updating object function with the minimum of natural frequency errors between the FE model prediction and the modal test data, model updating of the design combustor casing model based sensitivity analysis method was carried out using the experimental modal data. After model updating, the maximum frequency error of the first ten modes was decreased from 27.1% to 1.2%, compared with the test data. The result shows the effectiveness of the proposed method and certain significance in parameter selection for model updating.
机译:提出了一种基于模态应变能量变化的错误定位指示器,并用于选择在模型更新过程中更新的设计参数。采用空气发动机燃烧器壳体结构作为示例,使用测试数据建立并验证了燃烧器外壳的“超微模型”,并通过简化建模建立了减少的模型(也称为设计模型)。通过比较“超微模型”与燃烧器壳体的设计模型之间的模态应变能量变化,通过误差定位指示器突出了减小的燃烧器壳体建模的误差位置。然后,选择设计模型的更新参数作为基于误差定位指示符的模态应变能量变化的显着变化的区域。使用FE模型预测和模态测试数据之间的最小自然频率误差定义更新对象功能,使用实验模态数据进行设计燃烧器套管模型的设计燃烧器壳体模型的模型更新。与测试数据相比,模型更新后,前十种模式的最大频率误差从27.1%降至1.2%。结果显示了建议方法的有效性以及在模型更新的参数选择中的某些意义。

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