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基于CNN机翼气动系数预测
引用本文:吕召阳,聂雪媛,赵奥博.基于CNN机翼气动系数预测[J].北京航空航天大学学报,2023,49(3):674-680.
作者姓名:吕召阳  聂雪媛  赵奥博
作者单位:1.中国科学院 力学研究所,北京 100190
摘    要:随着机器学习的快速发展和其突出的非线性映射能力,越来越多的学者将机器学习方法应用到流体力学领域。为克服传统数学拟合不能很好的解决系统非线性问题,以及现有文献中所提及的一些基于神经网络的气动参数预测方法,需要进行参数化处理而带来的不便,同时为实现多变量多输出气动参数快速预测的目的,基于卷积神经网络考虑机翼变迎角和浮沉建立了一种多变量多输出的机翼气动参数预测模型,实现了机翼气动参数的快速预测。结果表明:所建模型具有较高且稳定的预测精度,并且计算效率较计算流体力学(CFD)提高了40倍。

关 键 词:卷积神经网络  机器学习  气动参数预测  气动降阶  深度学习
收稿时间:2021-05-27

Prediction of wing aerodynamic coefficient based on CNN
Institution:1.Institute of Mechanics,Chinese Academy of Sciences,Beijing 100190,China2.School of Engineering Science,University of Chinese Academy of Sciences,Beijing 100049,China
Abstract:With the rapid development of machine learning and its outstanding nonlinear mapping ability, more and more scholars apply machine learning methods to the field of fluid mechanics. To overcome the obstacle that the traditional mathematical fitting cannot well present the system nonlinearity and the inconvenience of some neural network-based aerodynamic parameter prediction methods due to the need of parametric processing, and to achieve the multi-variable and multi-output aerodynamic parameters, this paper establishes a multi-variable and multi-output model based on convolutional neural network considering the variable angle of attack and the heave of the wing to realize the rapid prediction of the aerodynamic coefficient of the wing. The results show that this model has high prediction accuracy and its computational efficiency is 40 times higher than computational fluid dynamics (CFD). Moreover, the designed stability experiment results show that the proposed model has good stability. 
Keywords:
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