机器学习预测气动失速

IF 1.1 4区 工程技术 Q4 MECHANICS International Journal of Computational Fluid Dynamics Pub Date : 2022-07-07 DOI:10.1080/10618562.2023.2171021
Ettore Saetta, R. Tognaccini, G. Iaccarino
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引用次数: 3

摘要

一个卷积自编码器是使用翼型空气动力学模拟的数据库进行训练,并在整体精度和可解释性方面进行评估。目标是预测失速,并调查的自编码器的能力,以区分翼型压力分布的线性和非线性响应,以改变迎角。在对学习基础结构进行敏感性分析后,我们研究了自编码器针对极端压缩率(即非常低维重建)识别的潜在空间。我们还提出了一种策略,使用解码器产生新的合成翼型几何形状和空气动力学的解决方案,通过插值和外推的潜在表征学习自编码器。
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Machine Learning to Predict Aerodynamic Stall
A convolutional autoencoder is trained using a database of airfoil aerodynamic simulations and assessed in terms of overall accuracy and interpretability. The goal is to predict the stall and to investigate the ability of the autoencoder to distinguish between the linear and non-linear response of the airfoil pressure distribution to changes in the angle of attack. After a sensitivity analysis of the learning infrastructure, we investigate the latent space identified by the autoencoder targeting extreme compression rates, i.e. very low-dimensional reconstructions. We also propose a strategy to use the decoder to generate new synthetic airfoil geometries and aerodynamic solutions by interpolation and extrapolation in the latent representation learned by the autoencoder.
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来源期刊
CiteScore
2.70
自引率
7.70%
发文量
25
审稿时长
3 months
期刊介绍: The International Journal of Computational Fluid Dynamics publishes innovative CFD research, both fundamental and applied, with applications in a wide variety of fields. The Journal emphasizes accurate predictive tools for 3D flow analysis and design, and those promoting a deeper understanding of the physics of 3D fluid motion. Relevant and innovative practical and industrial 3D applications, as well as those of an interdisciplinary nature, are encouraged.
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