Accurate evaluation of the Strouhal number is important for wind-resistant design, but traditional aerodynamic assessments are computationally expensive. To support rapid schematic design, this paper proposes a deep learning framework to predict the Strouhal number for 2D bluff bodies. Arbitrary irregular sections are represented using a unified three-channel geometric tensor that combines distance and spatial coordinate fields. A Residual Network integrated with Coordinate Attention, termed ResCA-Net, is developed to focus on vortex-shedding determinants, particularly leading-edge separation points. The model was trained on 1000 randomly generated convex sections, with target St values obtained from 2D URANS simulations at Re = 2 × 104. On an independent test set, ResCA-Net achieves an R2 of 0.9129, an MAE of 0.0316, and a median absolute percentage error of 6.56%. Systematic benchmarking shows that the embedded Coordinate Attention outperforms SE, CBAM, and the baseline ResNet. A single inference takes only 43.56 milliseconds, which is over 160,000 times faster than transient CFD simulations. This end-to-end method provides an efficient and accurate surrogate model for rapid iterative screening of aerodynamic shapes.
We introduce a dataset of approximately 10,000 Reynolds-Averaged Navier-Stokes (RANS) simulations of steady, incompressible, two-dimensional subsonic flow around downforce-generating NACA 4-digit airfoils, targeting aerodynamic regimes relevant to automotive and motorsport applications (openly available on https://hugg...
Haitz Sáez de Ocáriz Borde, Flavio Savarino, A. C. Popescu et al.· arXiv.org· 0 citations
High-fidelity Reynolds-averaged Navier--Stokes (RANS) simulations remain a standard tool for aerodynamic analysis, yet each solve on an unstructured mesh is computationally expensive, making many-query tasks such as design exploration, optimization, and multi-condition evaluation costly. Neural operators provide mesh-f...
Jun-Feng Chen, Yong-Chen Fan, Zhong-Hua Qiao et al.· 0 citations
To address the critical issues of low efficiency and lack of innovation in traditional aircraft aerodynamic shape design, this paper proposes an intelligent design method based on Wasserstein Generative Adversarial Network with Gradient Penalty (WGAN-GP) and TensorFlow 2.x. A foundational dataset containing 12,000 airf...
Shu-Kai Lin, Zhong-Hua Wen, Xiong Lin et al.· Journal of Physics, Conferen...· 0 citations
A combined field inversion and machine learning framework to enhance the Spalart–Allmaras turbulence model is employed, demonstrating a substantial improvement in pressure coefficient predictions for both in-sample and out-of-sample cases, without degrading the friction coefficient of a zero-pressure-gradient flat-plat...
Louis Carduner, B. Fanizza, F. Renac et al.· AIAA Journal· 0 citations
Accurate prediction of wind-induced interference effects in building groups is essential for wind-resistant design, yet traditional approaches based on computational fluid dynamics (CFD) or wind tunnel tests are prohibitively expensive for large-scale parametric investigations. This study presents a deep learning-aided...
Xiao-Wang Pan, Lian Shen, Ren-Ze Xu et al.· The Physics of Fluids· 0 citations
Thermal design and monitoring of compact heat exchangers require fields across changing operating conditions, and increasingly from a few embedded sensors, yet each new Reynolds number is a new mesh-based simulation. A physics-informed neural network (PINN) framework is presented for the coupled prediction and inverse...
Gaston Haidak, Jian-Long Kou, Dong-Yun Wang· The Physics of Fluids· 0 citations
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