用扩散模型生成满足气动要求的机翼形状,减少仿真次数。
Generative Aerodynamic Design with Diffusion Probabilistic Models
- 用扩散模型根据气动特性生成二维机翼,参数化保证平滑性。
- 相同条件下可生成多种候选设计,拓展优化起点。
- 数据集需包含未用于条件约束的物理约束,确保合理性。
气动外形优化通常依赖大量昂贵的仿真来评估和迭代改进几何形状。通过提供接近目标性能(如升力、阻力、气动矩、表面积)的初始形状,可减少仿真次数。本文展示生成模型具备提供此类初始形状的潜力,通过在大规模仿真数据集上训练扩散概率模型,实现基于给定气动特征与约束的二维机翼形状合成。机翼采用伯恩斯坦多项式参数化,确保生成设计的光滑性。结果表明,模型能在相同条件下生成多样化的候选设计,有效探索设计空间,为优化过程提供多个起点。但生成设计的质量取决于训练数据集中仿真设计的分布。关键在于训练数据中的几何形状必须满足未被模型条件化的其他物理约束,以确保生成结果的物理可行性。
原文摘要 · Abstract (English)
The optimization of geometries for aerodynamic design often relies on a large number of expensive simulations to evaluate and iteratively improve the geometries. It is possible to reduce the number of simulations by providing a starting geometry that has properties close to the desired requirements, often in terms of lift and drag, aerodynamic moments and surface areas. We show that generative models have the potential to provide such starting geometries by generalizing geometries over a large dataset of simulations. In particular, we leverage diffusion probabilistic models trained on XFOIL simulations to synthesize two-dimensional airfoil geometries conditioned on given aerodynamic features and constraints. The airfoils are parameterized with Bernstein polynomials, ensuring smoothness of the generated designs. We show that the models are able to generate diverse candidate designs for identical requirements and constraints, effectively exploring the design space to provide multiple starting points to optimization procedures. However, the quality of the candidate designs depends on the distribution of the simulated designs in the dataset. Importantly, the geometries in this dataset must satisfy other requirements and constraints that are not used in conditioning of the diffusion model, to ensure that the generated geometries are physical.
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