TL;DR
This paper introduces a novel aerodynamic surrogate modeling approach using $eta$-VAE architectures combined with PCA and Gaussian Process Regression to efficiently predict pressure distributions with high accuracy.
Contribution
It presents a new surrogate modeling framework leveraging $eta$-VAE, PCA, and Gaussian Process Regression for improved aerodynamic data prediction and interpretability.
Findings
Latent space correlates with flight conditions.
Regularization and PCA improve autoencoder performance.
Fine-tuning enhances model accuracy and reduces $eta$ dependence.
Abstract
Surrogate models that combine dimensionality reduction and regression techniques are essential to reduce the need for costly high-fidelity computational fluid dynamics data. New approaches using -Variational Autoencoder (-VAE) architectures have shown promise in obtaining high-quality low-dimensional representations of high-dimensional flow data while enabling physical interpretation of their latent spaces. We propose a surrogate model based on latent space regression to predict pressure distributions on a transonic wing given the flight conditions: Mach number and angle of attack. The -VAE model, enhanced with Principal Component Analysis (PCA), maps high-dimensional data to a low-dimensional latent space, showing a direct correlation with flight conditions. Regularization through requires careful tuning to improve overall performance, while PCA…
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Taxonomy
MethodsGaussian Process · Principal Components Analysis
