留言板

尊敬的读者、作者、审稿人, 关于本刊的投稿、审稿、编辑和出版的任何问题, 您可以本页添加留言。我们将尽快给您答复。谢谢您的支持!

姓名
邮箱
手机号码
标题
留言内容
验证码

基于深度学习的翼型反设计方法

何磊 钱炜祺 刘滔

何磊, 钱炜祺, 刘滔. 基于深度学习的翼型反设计方法[J]. 航空动力学报, 2020, 35(9): 1909-1917. doi: 10.13224/j.cnki.jasp.2020.09.013
引用本文: 何磊, 钱炜祺, 刘滔. 基于深度学习的翼型反设计方法[J]. 航空动力学报, 2020, 35(9): 1909-1917. doi: 10.13224/j.cnki.jasp.2020.09.013
HE Lei, QIAN Weiqi, LIU Tao. Inverse design method of airfoil based on deep learning[J]. Journal of Aerospace Power, 2020, 35(9): 1909-1917. doi: 10.13224/j.cnki.jasp.2020.09.013
Citation: HE Lei, QIAN Weiqi, LIU Tao. Inverse design method of airfoil based on deep learning[J]. Journal of Aerospace Power, 2020, 35(9): 1909-1917. doi: 10.13224/j.cnki.jasp.2020.09.013

基于深度学习的翼型反设计方法

doi: 10.13224/j.cnki.jasp.2020.09.013
基金项目: 国家自然科学基金(11802325); 中国空气动力研究与发展中心基础和前沿技术研究基金(FFTRF20172015)

Inverse design method of airfoil based on deep learning

  • 摘要: 建立了一种基于深度学习的翼型反设计方法,将翼型曲线及其对应的压力分布图像作为训练学习对象,建立其内在联系的模型,实现通过卷积神经网络提取压力分布图像的特征,计算获得翼型曲线。该方法直接将压力分布图像作为模型输入,更加直观简洁,同时避免了传统方法中耗时的数值计算过程。模型测试中,6 000组压力分布图像和翼型曲线用于模型训练,另外561组用于模型验证,验证耗时仅67 s,预测的翼型曲线与CFD计算结果的平均相对误差为055%。对比实验中,通过对压力分布曲线添加噪声、改变输出层尺寸等方式,进一步验证和分析了预测模型性能。结果表明该翼型反设计方法具有较高预测精度和较强鲁棒性,能在保证精度的情况下降低计算时间,提高设计效率。

     

  • [1] 王清,招启军.基于遗传算法的旋翼翼型综合气动优化设计[J].航空动力学报,2016,31(6):1486-1495. WANG Qing,ZHAO Qijun.Synthetical optimization design of rotor airfoil by genetic algorithm[J].Journal of Aerospace Power,2016,31(6):1486-1495.(in Chinese)
    [2] 高正红,王超.飞行器气动外形设计方法研究与进展[J].空气动力学学报,2017,35(4):516-528. GAO Zhenghong,WANG Chao.Aerodynamic shape design methods for aircraft:status and trends[J].Acta Aerodynamica Sinica,2017,35(4):516-528.(in Chinese)
    [3] 白俊强,邱亚松,华俊.改进型Gappy POD翼型反设计方法[J].航空学报,2013,34(4):762-771. BAI J Qunqiang,QIU Yasong,HUA Jun.Improved airfoil inverse design method based on Gappy POD[J].Acta Aeronautica et Astronautica Sinica,2013,34(4):762-771.(in Chinese)
    [4] 赵国庆,招启军.基于目标压力分布的旋翼先进气动外形反设计分析方法[J],航空学报,2014,35(3):744-755. ZHAO Guoqing,ZHAO Qijun.Inverse design analysis method on rotor with advanced aerodynamic configuration based upon target pressurse distribution[J].Acta Aeronautica et Astronautica Sinica,2014,35(3):744-755.(in Chinese)
    [5] LIGHTHILL M J.A new method of two-dimensional aerodynamics design[R].Aeronautical Research Council,ARC Technical Report No.2112,1945.
    [6] TAKANASHI S.Iterative three-dimensional transonic wing design using integral equations[J].Journal of Aircraft,1985,22(8):655-660.
    [7] 詹浩,华俊,张仲寅.基于余量修正原理的多翼面气动力反设计方法[J].航空学报,2003,24(5):411-413. ZHAN Hao,HUA Jun,ZHANG Zhongyin.Design of multi-lifting surfaces based on iterative residual correction[J].Acta Aeronautica et Astronautica Sinica,2003,24(5):411-413.(in Chinese)
    [8] 华俊,张仲寅.一种跨声速翼型设计方法及设计诸例[J].空气动力学学报,1990,8(2):117-123. HUA Jun,ZHANG Zhongyin.A Transonic airfoil design method and example[J].Acta Aerodynamica Sinica,1990,8(2):117-123.(in Chinese)
    [9] 李焦赞.基于目标压力分布优化翼型反设计方法研究[D].西安:西北工业大学,2007. LI Jiaozan.Study on inverse design method of airfoil based on optimization of target pressure distribution[D].Xi’an:Northwestern Polytechnical University,2007.(in Chinese)
    [10] 赵小虎,阎超.基于气动数值模拟的翼型反设计方法[J].航空学报,1997,18(6):9-12. ZHAO Xiaohu,YAN Chao.Aerodynamic inverse design method of airfoil via CFD[J].Acta Aeronautica et Astronautica Sinica,1997,18(6):9-12.(in Chinese)
    [11] BUI-THANH T,DAMODARAN M,WILLCOX K.Aerodynamic data reconstruction and inverse design using proper orthogonal decomposition[J].AIAA Journal,2004,42(8):1501-1516.
    [12] 刘俊,宋文萍,韩忠华.Kriging模型在翼型反设计中的应用研究[J].空气动力学学报,2014,32(4):518-526. LIU Jun,SONG Wenping,HAN Zhonghua,et al.Kriging-based airfoil inverse design[J].Acta Aerodynamica Sinica,2014,32(4):518-526.(in Chinese)
    [13] 韩少强,宋文萍,韩忠华,等.基于梯度增强型Kriging模型的气动反设计方法[J].航空学报,2017,38(7):138-152. HAN Shaoqiang,SONG Wenping,HAN Zhonghua,et al.Aerodynamic inverse design method based on gradient-enhanced Kriging model[J].Acta Aeronautica et Astronautica Sinica,2017,38(7):138-152.(in Chinese)
    [14] 詹浩,朱军,白俊强,等.遗传算法结合反设计的翼型优化设计研究[J].西北工业大学学报,2006,24(5):541-543. ZHAN Hao,ZHU Jun,BAI Junqiang,et al.Improving design of airfoil with genetic algorithm (GA) combined with inverse design method[J].Journal of Northwestern Polytechnical University,2006,24(5):541-543.(in Chinese)
    [15] 李秀娟,廖文和,刘浩.基于翼型反设计的遗传算法[J].南京航空航天大学学报,2007,39(2):263-266. LI Xiujuan,LIAO Wenhe,LIU Hao.Genetic algorithms based on airfoil inverse design[J].Journal of Nanjing University of Aeronautics and Astronautics,2007,39(2):263-266.(in Chinese)
    [16] WANG X,DAMODARAN M,LEE S L.Inverse transonic airfoil design using parallel simulated annealing and computational fluid dynamics[J].AIAA Journal,2002,40(4):791-794.
    [17] 单志辉.基于高斯过程回归的翼型快速设计研究[D].南京:南京航空航天大学,2011. SHAN Zhihui.Fast airfoil design based on gaussian process regression[D].Nanjing:Nanjing University of Aeronautics and Astronautics,2011.(in Chinese)
    [18] 刘凌君,周越,高振勋.基于神经网络的翼型气动力计算和反设计方法[J].气体物理,2018,3(5):43-49. LIU Lingjun,ZHOU Yue,GAO Zhenxun.Aerodynamic force calculation and inverse design for airfoil based on neural network[J].Physics of Gases,2018,3(5):41-47.(in Chinese)
    [19] SUN G,SUN Y,WANG S.Artificial neural network based inverse design:airfoils and wings[J].Aerospace Science and Technology,2015,42:415-428.
    [20] SOBIECZKY H.Parametric airfoils and wings[C]∥Proceedings of Recent Development of Aerodynamic Design Methodologies.Berlin:Vieweg Teubner Verlag,1999:71-87.
    [21] 张德虎,席胜,田鼎.典型翼型参数化方法的翼型外形控制能力评估[J].航空工程进展,2014,5(3):281-288. ZHANG Dehu,XI Sheng,TIAN Ding.Geometry control ability evaluation of classical airfoil parametric methods[J].Advance in Aeronautical Science And Engineering,2014,5(3):281-288.(in Chinese)
    [22] SAMAREH J A,SAMAREH J A,POLYNOMIAL B B.A survey of shape parameterization techniques[R].NASA/CP-1999-209136,1999.
    [23] HINTON G E,SALAKHUTDINOV R R.Reducing the dimensionality of data with neural networks[J].Science,2006,313(5786):504-507.
    [24] 吴正文.卷积神经网络在图像分类中的应用研究[D].成都:电子科技大学,2015. WU Zhengwen.Application research of convolution neural network in image classification[D].Chengdu:University of Electronic Science and Technology,2015.(in Chinese)
    [25] 袁江林,郭志刚,陈刚,等.基于深度学习的文本自动生成技术研究综述[J].信息工程大学学报,2018,19(5):616-620. YUAN Jianglin,GUO Zhigang,CHEN Gang,et al.Summary of text auto-generation technology research based on deep learning[J].Journal of Information Engineering University,2018,19(5):616-620.(in Chinese)
    [26] FRANK S,GANG L,Dong Y.Conversational speech transcription using context-dependent deep neural networks[R].Florence,Italy:the 12th Annual Conference of the International Speech Communication Association,2011.
    [27] 陈海,钱炜祺,何磊.基于深度学习的翼型气动系数预测[J].空气动力学学报,2018,36(2):294-299. CHEN Hai,QIAN Weiqi,HE Lei.Aerodynamic coefficient prediction of airfoils based on deep learning[J].Acta Aerodynamica Sinica,2018,36(2):294-299.(in Chinese)
    [28] 廖鹏,姚磊江,白国栋,等.基于深度学习的混合翼型前缘压力分布预测[J].航空动力学报,2019,34(8):1751-1758. LIAO Peng,YAO Leijiang,BAI Guodong,et al.Prediction of hybrid airfoil leading edge pressure distribution based on deep learning[J].Journal of Aerospace Power,2019,34(8):1751-1758.(in Chinese)
    [29] LEE S,YOU D.Data-driven prediction of unsteady flow over a circular cylinder using deep learning[J].Journal of Fluid Mechanics,2019,879:217-254.
    [30] 李彦冬,郝宗波,雷航.卷积神经网络研究综述[J].计算机应用,2016,36(9):2508-2515. LI Yandong,HAO Zongbo,LEI Hang.Survey of convolutional neural network[J].Journal of Computer Applications,2016,36(9):2508-2515.(in Chinese)
    [31] LECUN Y,BOTTOU L,BENGIO Y,et al.Gradient-based learning applied to document recognition[J].Proceedings of the IEEE,1998,86(11):2278-2324.
    [32] LECUN Y,BENGIO Y,HINTON G.Deep learning[J].Nature,2015,521(7553):436-446.
    [33] GLOROT X,BENGIO Y.Understanding the difficulty of training deep feedforward neural networks[R].Brookline,MA,USA:International Conference on Artificial Intelligence and Statistics,2010.
    [34] NAIR V,HINTON G E.Rectified linear units improve restricted Boltzmann machines[C]∥Proceedings of the 27th International Conference on Machine Learning.Haifa,Israel:Omni Press,2010:807-814.
    [35] KRiZHEVSKY A,SUTSKEVER I,HINTON G E.Imagenet classificationwith deep convolutional neural networks[C]∥Advances in Neural Information Processing Systems.New York:Curran Associates,2012:1097-1105.
    [36] 王建军,高正红.HicksHenne翼型参数化方法分析及改进[J].航空计算技术,2010,40(4):46-49. WANG Jianjun,GAO Zhenghong.Analysis and improvement of hickshenne airfoil parameterization method[J].Aeronautical Computing Technique,2010,40(4):46-49.(in Chinese)
    [37] 陈作斌,江雄,周铸,等.计算流体技术及应用[J].中国科学:E辑,2008,38(5):657-670. CHEN Zuobin,JIANG Xiong,ZHOU Zhu,et al.Computational fluid technology and application[J].Science in China:E,2008,38(5):657-670.(in Chinese)
    [38] 王建涛,易贤,肖中云,等.ARJ21-700飞机冰脱落数值模拟[J].空气动力学学报,2013,31(4):430-436. WANG Jiantao,YI Xian,XIAO Zhongyun,et al.Numerical simulation of ice shedding from ARJ21-700[J].Acta Aerodynamica Sinica,2013,31(4):430-436.(in Chinese)
    [39] KINGMA D P,BA J.Adam:a method for stochastic optimization[R].San Diego,USA:the 3rd International Conference for Learning Representations,2015.
  • 加载中
计量
  • 文章访问数:  224
  • HTML浏览量:  4
  • PDF量:  269
  • 被引次数: 0
出版历程
  • 收稿日期:  2020-03-15
  • 刊出日期:  2020-09-28

目录

    /

    返回文章
    返回