Study of transfer learning from 2D supercritical airfoils to 3D transonic swept wings
Runze Li, Yufei Zhang, Haixin Chen

TL;DR
This study demonstrates that transfer learning from 2D supercritical airfoil models can effectively predict 3D swept wing flows, significantly reducing sample requirements and prediction errors in fluid mechanics applications.
Contribution
The paper introduces a transfer learning approach that reuses 2D models for 3D wing predictions, embedding swept theory to enhance accuracy and reduce data needs.
Findings
Transfer learning achieves good accuracy with ~500 samples.
Transferred models reduce prediction errors by 60% and 80%.
Embedding swept theory improves 3D flow predictions.
Abstract
Machine learning has been widely utilized in fluid mechanics studies and aerodynamic optimizations. However, most applications, especially flow field modeling and inverse design, involve two-dimensional flows and geometries. The dimensionality of three-dimensional problems is so high that it is too difficult and expensive to prepare sufficient samples. Therefore, transfer learning has become a promising approach to reuse well-trained two-dimensional models and greatly reduce the need for samples for three-dimensional problems. This paper proposes to reuse the baseline models trained on supercritical airfoils to predict finite-span swept supercritical wings, where the simple swept theory is embedded to improve the prediction accuracy. Two baseline models for transfer learning are investigated: one is commonly referred to as the forward problem of predicting the pressure coefficient…
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Taxonomy
TopicsModel Reduction and Neural Networks · Fluid Dynamics and Turbulent Flows · Aerodynamics and Acoustics in Jet Flows
