Multifidelity Aerodynamic Data Fusion by Autoencoder Transfer Learning

Accurate aerodynamic prediction often relies on high-fidelity (HF) simulations; however, their prohibitive computational costs severely limit their applicability in data-driven modeling. This limitation motivates the development of multifidelity strategies that leverage inexpensive low-fidelity (LF) information without compromising accuracy. Addressing this challenge, this work presents a multifidelity deep learning framework that combines autoencoder-based transfer learning with a newly developed multisplit conformal prediction (MSCP) strategy to achieve uncertainty-aware aerodynamic data fusion under extreme data scarcity. The methodology leverages abundant LF data to learn a compact latent physics representation, which acts as a frozen knowledge base for a decoder that is subsequently fine-tuned using scarce HF samples. Tested on surface-pressure distributions for NACA airfoils (two-dimensional) and a transonic wing (three-dimensional) databases, the model successfully corrects LF deviations and achieves high-accuracy pressure predictions using minimal HF training data. Furthermore, the MSCP framework produces robust, actionable uncertainty bands with pointwise coverage exceeding 95%. By combining extreme data efficiency with uncertainty quantification, this work offers a scalable and reliable solution for aerodynamic regression in data-scarce environments.

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Publication Details

Journal
AIAA Journal
Published
2026-11-02
DOI
https://doi.org/10.2514/1.j066795
Primary Topic
Model Reduction and Neural Networks
Type
article
Field-Weighted Citation Impact
0.00

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article

Multifidelity Aerodynamic Data Fusion by Autoencoder Transfer Learning

Rodrigo Castellanos, E. Andrés, Javier Nieto-Centenero
5 links
AIAA Journal
Model Reduction and Neural Networks
article

Multifidelity Aerodynamic Data Fusion by Autoencoder Transfer Learning

Rodrigo Castellanos, E. Andrés, Javier Nieto-Centenero
article en

Abstract

Accurate aerodynamic prediction often relies on high-fidelity (HF) simulations; however, their prohibitive computational costs severely limit their applicability in data-driven modeling. This limitation motivates the development of multifidelity strategies that leverage inexpensive low-fidelity (LF) information without compromising accuracy. Addressing this challenge, this work presents a multifidelity deep learning framework that combines autoencoder-based transfer learning with a newly developed multisplit conformal prediction (MSCP) strategy to achieve uncertainty-aware aerodynamic data fusion under extreme data scarcity. The methodology leverages abundant LF data to learn a compact latent physics representation, which acts as a frozen knowledge base for a decoder that is subsequently fine-tuned using scarce HF samples. Tested on surface-pressure distributions for NACA airfoils (two-dimensional) and a transonic wing (three-dimensional) databases, the model successfully corrects LF deviations and achieves high-accuracy pressure predictions using minimal HF training data. Furthermore, the MSCP framework produces robust, actionable uncertainty bands with pointwise coverage exceeding 95%. By combining extreme data efficiency with uncertainty quantification, this work offers a scalable and reliable solution for aerodynamic regression in data-scarce environments.

AIAA Journal
Instituto Nacional de Técnica Aeroespacial (ES), Universidad Carlos III de Madrid (ES)
Agencia Estatal de Investigación
Openalex Percentile: Top 98%
Model Reduction and Neural Networks
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