基于 Airfoil-DDPM 的无参数函数翼型生成方法

Airfoil-DDPM: A non-parametric diffusion-based framework for airfoil generation

  • 摘要: 本文提出了一种基于去噪扩散概率模型(denoising diffusion probabilistic models, DDPM)的翼型生成方 法 Airfoil- DDPM,旨在提高翼型设计的效率和灵活性。该方法利用扩散模型直接学习翼型几何特征并生成翼型,无需依赖传统参数化方法,从而避免预设参数函数对形状多样性的限制。通过结合 UNet 和注意力机制,模型能够精确捕捉训练样本的几何细节,生成具有光滑表面和连续曲率的翼型。实验表明,Airfoil-DDPM在生成 NACA0012 和 RAE2822 翼型时,不仅能够保持几何表征精度,还能满足气动力性能需求。可视化分析进一步验证了该方法在UIUC 数据集上的分布学习能力,展示了其在设计多样性上的显著优势。本研究为翼型生成提供了一种高效且灵活的无参数化解决方案,有助于推动飞行器设计与优化的发展。

     

    Abstract: Accurate and flexible geometric parameterization is a cornerstone of modern aerodynamic design and optimization. While recent advances in generative modelling have improved airfoil design workflows by learning latent representations, most existing approaches still rely on traditional parametric functions, which inherently constrain the design space and limit geometric diversity. To overcome these limitations, we propose Airfoil-DDPM, a non-parametric airfoil generation framework based on Denoising Diffusion Probabilistic Models (DDPM). Our method directly learns the geometric distribution of airfoil shapes from data and generates high-fidelity designs without any predefined parameterization. By integrating a UNet backbone with attention mechanisms, Airfoil-DDPM captures fine-scale geometric features and ensures smoothness and curvature continuity. Experimental results demonstrate that Airfoil-DDPM accurately reproduces both the geometric and aerodynamic characteristics of standard airfoils such as NACA0012 and RAE2822. Furthermore, qualitative visualizations confirm its superior ability to learn the UIUC library’s data distribution and generate diverse, physically plausible airfoil geometries. Our approach offers a flexible and efficient alternative to traditional parameterization-based methods, paving the way for next-generation aerodynamic design.

     

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