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Application of a PCA-DBN-based surrogate model to robust aerodynamic design optimization
作者姓名:Jun TAO  Gang SUN  Liqiang GUO  Xinyu WANG
作者单位:1. Department of Aeronautics & Astronautics, Fudan University;2. Department of Mechanical & Aerospace Engineering, University of California
基金项目:co-supported by Aeronautical Science Foundation of China (No. 2015ZBP9002);;China Scholarship Council;
摘    要:An efficient method employing a Principal Component Analysis(PCA)-Deep Belief Network(DBN)-based surrogate model is developed for robust aerodynamic design optimization in this study. In order to reduce the number of design variables for aerodynamic optimizations, the PCA technique is implemented to the geometric parameters obtained by parameterization method.For the purpose of predicting aerodynamic parameters, the DBN model is established with the reduced design variables as input and the aero...

收稿时间:20 March 2019

Application of a PCA-DBN-based surrogate model to robust aerodynamic design optimization
Jun TAO,Gang SUN,Liqiang GUO,Xinyu WANG.Application of a PCA-DBN-based surrogate model to robust aerodynamic design optimization[J].Chinese Journal of Aeronautics,2020,33(6):1573-1588.
Institution:1. Department of Aeronautics & Astronautics, Fudan University, Shanghai 200433, China;2. Department of Mechanical & Aerospace Engineering, University of California, Irvine 92697, USA
Abstract:An efficient method employing a Principal Component Analysis (PCA)-Deep Belief Network (DBN)-based surrogate model is developed for robust aerodynamic design optimization in this study. In order to reduce the number of design variables for aerodynamic optimizations, the PCA technique is implemented to the geometric parameters obtained by parameterization method. For the purpose of predicting aerodynamic parameters, the DBN model is established with the reduced design variables as input and the aerodynamic parameters as output, and it is trained using the k-step contrastive divergence algorithm. The established PCA-DBN-based surrogate model is validated through predicting lift-to-drag ratios of a set of airfoils, and the results indicate that the PCA-DBN-based surrogate model is reliable and obtains more accurate predictions than three other surrogate models. Then the efficient optimization method is established by embedding the PCA-DBN-based surrogate model into an improved Particle Swarm Optimization (PSO) framework, and applied to the robust aerodynamic design optimizations of Natural Laminar Flow (NLF) airfoil and transonic wing. The optimization results indicate that the PCA-DBN-based surrogate model works very well as a prediction model in the robust optimization processes of both NLF airfoil and transonic wing. By employing the PCA-DBN-based surrogate model, the developed efficient method improves the optimization efficiency obviously.
Keywords:Aerodynamic design optimization  Deep neural networks  Particle swarm optimization  Principal component analysis  Surrogate model
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