Physics-Regularized Generative Parameterization for Efficient Aerodynamic Shape Optimization

Aircraft design involves optimization within extremely high-dimensional geometric design spaces, posing a fundamental challenge for aerodynamic shape optimization. Although geometric filtering has improved design-space compactness compared to conventional parameterization methods, a compelling need remains to further shrink the design space without sacrificing design quality. This study introduces a physics-regularized generative parameterization that integrates data-driven aerodynamic modeling with generative learning to achieve a compact space for aerodynamic shape optimization. The approach begins by constructing a modal design space via deep-learning-based geometric filtering. A self-evolving aerodynamic modeling framework with adaptive sampling is then developed to efficiently introduce physical regularization. An optimization-based sampling method is proposed to generate a diverse set of feasible aerodynamic shapes under both geometric and performance constraints. A generative model trained on this physics-regularized database provides a low-dimensional latent space for shape optimization. Validation on blended-wing-body configurations demonstrates that the proposed method maintains geometric completeness while reducing design variables by [Formula: see text] relative to the state-of-the-art geometric filtering. Consequently, the surrogate-based optimization cost decreases by over 55%, and the drag prediction error in fast data-driven optimization drops from 32.5 to 3.2%. These results confirm that the proposed physics-regularized generative parameterization enables a compact geometric space to effectively meet various aircraft design requirements.

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Publication Details

Journal
AIAA Journal
Published
2026-04-24
DOI
https://doi.org/10.2514/1.j066536
Primary Topic
Topology Optimization in Engineering
Type
article
Field-Weighted Citation Impact
0.00

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article

Physics-Regularized Generative Parameterization for Efficient Aerodynamic Shape Optimization

Mengying Ma, Jichao Li, Xiangyu Gu, Xinwei Wang
AIAA Journal
Topology Optimization in Engineering
article

Physics-Regularized Generative Parameterization for Efficient Aerodynamic Shape Optimization

Mengying Ma, Jichao Li, Xiangyu Gu, Xinwei Wang
article en

Abstract

Aircraft design involves optimization within extremely high-dimensional geometric design spaces, posing a fundamental challenge for aerodynamic shape optimization. Although geometric filtering has improved design-space compactness compared to conventional parameterization methods, a compelling need remains to further shrink the design space without sacrificing design quality. This study introduces a physics-regularized generative parameterization that integrates data-driven aerodynamic modeling with generative learning to achieve a compact space for aerodynamic shape optimization. The approach begins by constructing a modal design space via deep-learning-based geometric filtering. A self-evolving aerodynamic modeling framework with adaptive sampling is then developed to efficiently introduce physical regularization. An optimization-based sampling method is proposed to generate a diverse set of feasible aerodynamic shapes under both geometric and performance constraints. A generative model trained on this physics-regularized database provides a low-dimensional latent space for shape optimization. Validation on blended-wing-body configurations demonstrates that the proposed method maintains geometric completeness while reducing design variables by [Formula: see text] relative to the state-of-the-art geometric filtering. Consequently, the surrogate-based optimization cost decreases by over 55%, and the drag prediction error in fast data-driven optimization drops from 32.5 to 3.2%. These results confirm that the proposed physics-regularized generative parameterization enables a compact geometric space to effectively meet various aircraft design requirements.

AIAA Journal
Northwestern Polytechnical University (CN), China Academy of Launch Vehicle Technology (CN)
National Natural Science Foundation of China
Openalex Percentile: Top 7%
Topology Optimization in Engineering
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