High-dimensional aerodynamic data modeling using a machine learning method based on a convolutional neural network

被引:0
作者
Bo-Wen Zan
Zhong-Hua Han
Chen-Zhou Xu
Ming-Qi Liu
Wen-Zheng Wang
机构
[1] Institute of Aerodynamic and Multidisciplinary Design Optimization,Aircraft Swarm Intelligent Sensing and Cooperative Control Key Laboratory of Sichuan Province, School of Aeronautics and Astronautics
[2] National Key Laboratory of Science and Technology On Aerodynamic Design and Research,undefined
[3] School of Aeronautics,undefined
[4] Northwestern Polytechnical University,undefined
[5] University of Electronic Science and Technology of China,undefined
来源
Advances in Aerodynamics | / 4卷
关键词
Aerodynamic data modeling; High-dimensional problem; Machine learning; Convolutional neural network; Computational fluid dynamics;
D O I
暂无
中图分类号
学科分类号
摘要
Modeling high-dimensional aerodynamic data presents a significant challenge in aero-loads prediction, aerodynamic shape optimization, flight control, and simulation. This article develops a machine learning approach based on a convolutional neural network (CNN) to address this problem. A CNN can implicitly distill features underlying the data. The number of parameters to be trained can be significantly reduced because of its local connectivity and parameter-sharing properties, which is favorable for solving high-dimensional problems in which the training cost can be prohibitive. A hypersonic wing similar to the Sanger aerospace plane carrier wing is employed as the test case to demonstrate the CNN-based modeling method. First, the wing is parameterized by the free-form deformation method, and 109 variables incorporating flight status and aerodynamic shape variables are defined as model input. Second, more than 7000 sample points generated by the Latin hypercube sampling method are evaluated by performing computational fluid dynamics simulations using a Reynolds-averaged Navier–Stokes flow solver to obtain an aerodynamic database, and a CNN model is built based on the observed data. Finally, the well-trained CNN model considering both flight status and shape variables is applied to aerodynamic shape optimization to demonstrate its capability to achieve fast optimization at multiple flight statuses.
引用
收藏
相关论文
共 95 条
[1]  
Pamadi BN(2001)Aerodynamic characteristics, database development, and flight simulation of the X-34 vehicle J Spacecraft Rockets 38 334-344
[2]  
Brauckmann GJ(2005)Three-dimensional aerodynamic mathematical model for tactical missiles with jet steering Aerospace Shanghai 22 13-18
[3]  
Ruth MJ(2004)Mathematic modeling for the missile aerodynamics with tail-wing according to wind-tunnel test results Experiments and Measurements in Fluid Mechanics 18 62-66
[4]  
Fu JM(2013)Transonic aerodynamic load modeling of X-31 aircraft pitching motions AIAA J 51 2447-2464
[5]  
He KF(1951)A statistical approach to some basic mine valuation problems on the Witwatersrand J Chem Metall Min Soc South Afr 52 119-139
[6]  
Wang WZ(2012)Hierarchical kriging model for variable-fidelity surrogate modeling AIAA J 50 1885-1896
[7]  
Qian WQ(2013)Improving variable-fidelity surrogate modeling via gradient-enhanced kriging and a generalized hybrid bridge function Aerosp Sci Technol 25 177-189
[8]  
Ghoreyshi M(2017)Efficient aerodynamic shape optimization of transonic wings using a parallel infilling strategy and surrogate models Struct Multidiscip O 55 925-943
[9]  
Cummings RM(2012)The research of RBFNN in modeling of nonlinear unsteady aerodynamics Acta Aerodyn Sin 30 108-112+119
[10]  
Da Ronch A(2013)Application of support vector regression for aerodynamic modeling Computer Simulation 30 128-132