Towards scalable surrogate models based on neural fields for large scale aerodynamic simulations

• Neural field surrogate for large-scale CFD problems • Discretization invariant, encoder-decoder architecture • Handles non-parametric geometric variability in 2D and 3D • Efficient geometry encoding of Signed Distance Function via metalearning • Achieves state-of-the-art performance vs. prior surrogates This paper introduces a novel surrogate modeling framework for aerodynamic applications based on Neural Fields. The proposed approach, MARIO (Modulated Aerodynamic Resolution Invariant Operator), addresses non parametric geometric variability through an efficient shape encoding mechanism and exploits the discretization-invariant nature of Neural Fields. It enables training on significantly downsampled meshes, while maintaining consistent accuracy during full-resolution inference. These properties allow for efficient modeling of diverse flow conditions, while reducing computational cost and memory requirements compared to traditional CFD solvers and existing surrogate methods. The framework is validated on two complementary datasets that reflect industrial constraints. First, the AirfRANS dataset consists of a two-dimensional airfoil benchmark with non-parametric shape variations. Performance evaluation of MARIO on this case demonstrates an order of magnitude improvement in prediction accuracy over existing methods across velocity, pressure, and turbulent viscosity fields, while accurately capturing boundary layer phenomena and aerodynamic coefficients. Second, the NASA Common Research Model features three-dimensional pressure distributions on a full aircraft surface mesh, with parametric control surface deflections. This configuration confirms MARIO’s accuracy and scalability. Benchmarking against state-of-the-art methods demonstrates that Neural Field surrogates can provide rapid and accurate aerodynamic predictions under the computational and data limitations characteristic of industrial applications.

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Publication Details

Journal
Computers & Fluids
Published
2025-11-27
DOI
https://doi.org/10.1016/j.compfluid.2025.106929
Primary Topic
Model Reduction and Neural Networks
Type
article
Field-Weighted Citation Impact
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article

Towards scalable surrogate models based on neural fields for large scale aerodynamic simulations

Michaël Bauerheim, Joseph Morlier, Xavier Bertrand, G. Catalani et al.
Computers & Fluids
Model Reduction and Neural Networks
article

Towards scalable surrogate models based on neural fields for large scale aerodynamic simulations

Michaël Bauerheim, Joseph Morlier, Xavier Bertrand, G. Catalani, Frédéric Tost, Jean Fesquet
article en

Abstract

• Neural field surrogate for large-scale CFD problems • Discretization invariant, encoder-decoder architecture • Handles non-parametric geometric variability in 2D and 3D • Efficient geometry encoding of Signed Distance Function via metalearning • Achieves state-of-the-art performance vs. prior surrogates This paper introduces a novel surrogate modeling framework for aerodynamic applications based on Neural Fields. The proposed approach, MARIO (Modulated Aerodynamic Resolution Invariant Operator), addresses non parametric geometric variability through an efficient shape encoding mechanism and exploits the discretization-invariant nature of Neural Fields. It enables training on significantly downsampled meshes, while maintaining consistent accuracy during full-resolution inference. These properties allow for efficient modeling of diverse flow conditions, while reducing computational cost and memory requirements compared to traditional CFD solvers and existing surrogate methods. The framework is validated on two complementary datasets that reflect industrial constraints. First, the AirfRANS dataset consists of a two-dimensional airfoil benchmark with non-parametric shape variations. Performance evaluation of MARIO on this case demonstrates an order of magnitude improvement in prediction accuracy over existing methods across velocity, pressure, and turbulent viscosity fields, while accurately capturing boundary layer phenomena and aerodynamic coefficients. Second, the NASA Common Research Model features three-dimensional pressure distributions on a full aircraft surface mesh, with parametric control surface deflections. This configuration confirms MARIO’s accuracy and scalability. Benchmarking against state-of-the-art methods demonstrates that Neural Field surrogates can provide rapid and accurate aerodynamic predictions under the computational and data limitations characteristic of industrial applications.

Computers & FluidsVol. 306
Airbus (France) (FR), Centre National de la Recherche Scientifique (FR), Université Toulouse III - Paul Sabatier (FR), Université Fédérale de Toulouse Midi-Pyrénées (FR), Institut Superieur de l'Aeronautique et de l'Espace (ISAE-SUPAERO) (FR), Institut National des Sciences Appliquées de Toulouse (FR), Institut Clément Ader (FR)
Openalex Percentile: Top 71%
Model Reduction and Neural Networks
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