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基于POD-BPNN的热启动策略及其在气动代理优化中的应用
引用本文:贾续毅,李春娜,常琦,季稳. 基于POD-BPNN的热启动策略及其在气动代理优化中的应用[J]. 航空工程进展, 2022, 13(5): 59-68
作者姓名:贾续毅  李春娜  常琦  季稳
作者单位:西北工业大学航天学院,西北工业大学航天学院,火箭军装备部装备项目管理中心,西北工业大学航天学院
摘    要:传统气动优化设计需要大量CFD 分析,而代理优化(SBO)方法能够有效降低CFD 分析次数,但该方法并没有改变单个CFD 分析时间。提出一种基于本征正交分解-反向传播神经网络(POD-BPNN)模型的热启动策略,并应用于气动代理优化。使用POD-BPNN 模型对SBO 中的初始样本建立从几何设计变量到流场数据的预测模型...

关 键 词:POD  BPNN  热启动  气动优化  翼型设计
收稿时间:2021-11-02
修稿时间:2022-02-04

The hot-start strategy based on POD-BPNN and its application in aerodynamic shape optimization using surrogate-based approach
Jiaxuyi,Lichunn,Changqi and Jiwen. The hot-start strategy based on POD-BPNN and its application in aerodynamic shape optimization using surrogate-based approach[J]. Advances in Aeronautical Science and Engineering, 2022, 13(5): 59-68
Authors:Jiaxuyi  Lichunn  Changqi  Jiwen
Affiliation:School of Astronautics, Northwestern Polytechnical University,School of Astronautics, Northwestern Polytechnical University,,
Abstract:Traditional aerodynamic optimization design requires multiple time-consuming CFD analyses; while widely-used surrogate-based optimization (SBO) can effectively reduce the number of CFD analyses, but it cannot speed up a single CFD analysis. Hence, this paper proposes a hot-start strategy using the proper orthogonal decomposition-back propagation based neural network (POD-BPNN), and applies it in surrogate-based aerodynamic optimization. First, the POD-BPNN model is built from geometric design variables to flowfield data through the initial samples in an SBO. Then, during iteration of the SBO, the flowfield of a new sample is predicted by the built model, and is used as the initial flowfield of the hot-start CFD analysis for the new sample. At the same time, the new sample is used to update the POD-BPNN model until the end of the optimization. The results of the aerodynamic optimization design of the transonic airfoil indicate: the hot-start strategy using the POD-BPNN can reduce the time of a single CFD analysis by 68%, and improves the efficiency of the SBO by 37%.
Keywords:POD   BPNN   hot-start   aerodynamic optimization   airfoil design
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