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Generative Aerodynamic Design with Diffusion Probabilistic Models

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arxiv 2409.13328 v1 pith:WL5LWXAN submitted 2024-09-20 cs.CE cs.LG

classification cs.CEcs.LG
keywords geometriesaerodynamicdesignsmodelssimulationsconstraintsdatasetdesign
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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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Cited by 2 Pith papers

Reviewed papers in the Pith corpus that reference this work. Sorted by Pith novelty score. Full citation record

  1. Efficient Diffusion Models under Nonconvex Equality and Inequality constraints via Landing

    cs.LG 2026-04 unverdicted novelty 7.0 of 10

    Landing-based constrained Langevin dynamics (overdamped and underdamped) replace per-step projections in diffusion models on nonconvex feasible sets, achieving comparable sample quality at up to 47x lower sampling cost.

  2. Adjoint-Based Aerodynamic Shape Optimization with a Manifold Constraint Learned by Diffusion Models

    cs.CE 2025-07 conditional novelty 6.0 of 10

    Airfoil drag minimization is reformulated as optimization in the latent space of a diffusion model, with CFD adjoint gradients backpropagated through the diffusion sampler; the approach beats a Hicks-Henne baseline in...

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