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Multi-Fidelity Bayesian Neural Network for Uncertainty Quantification in Transonic Aerodynamic Loads

Andrea Vaiuso, Gabriele Immordino, Marcello Righi, Andrea Da Ronch

TL;DR

Addressing uncertainty in transonic aerodynamic loads with multi-fidelity data, the paper develops MF-BayNet, a transfer-learning-enabled Bayesian neural network framework. It pre-trains on low-fidelity data, then sequentially fine-tunes on mid- and high-fidelity data, using Monte Carlo sampling to obtain predictive means and uncertainties. The authors show MF-BayNet outperforms Co-Kriging on $C_L$ and $C_M$ with about half the error and tighter uncertainty bounds, validating the approach for aerospace applications with limited high-fidelity data. The work contributes a transparent, open-source framework for uncertainty-aware multi-fidelity learning in transonic aerodynamics.

Abstract

Multi-fidelity models are becoming more prevalent in engineering, particularly in aerospace, as they combine both the computational efficiency of low-fidelity models with the high accuracy of higher-fidelity simulations. Various state-of-the-art techniques exist for fusing data from different fidelity sources, including Co-Kriging and transfer learning in neural networks. This paper aims to implement a multi-fidelity Bayesian neural network model that applies transfer learning to fuse data generated by models at different fidelities. Bayesian neural networks use probability distributions over network weights, enabling them to provide predictions along with estimates of their confidence. This approach harnesses the predictive and data fusion capabilities of neural networks while also quantifying uncertainty. The results demonstrate that the multi-fidelity Bayesian model outperforms the state-of-the-art Co-Kriging in terms of overall accuracy and robustness on unseen data.

Multi-Fidelity Bayesian Neural Network for Uncertainty Quantification in Transonic Aerodynamic Loads

TL;DR

Addressing uncertainty in transonic aerodynamic loads with multi-fidelity data, the paper develops MF-BayNet, a transfer-learning-enabled Bayesian neural network framework. It pre-trains on low-fidelity data, then sequentially fine-tunes on mid- and high-fidelity data, using Monte Carlo sampling to obtain predictive means and uncertainties. The authors show MF-BayNet outperforms Co-Kriging on and with about half the error and tighter uncertainty bounds, validating the approach for aerospace applications with limited high-fidelity data. The work contributes a transparent, open-source framework for uncertainty-aware multi-fidelity learning in transonic aerodynamics.

Abstract

Multi-fidelity models are becoming more prevalent in engineering, particularly in aerospace, as they combine both the computational efficiency of low-fidelity models with the high accuracy of higher-fidelity simulations. Various state-of-the-art techniques exist for fusing data from different fidelity sources, including Co-Kriging and transfer learning in neural networks. This paper aims to implement a multi-fidelity Bayesian neural network model that applies transfer learning to fuse data generated by models at different fidelities. Bayesian neural networks use probability distributions over network weights, enabling them to provide predictions along with estimates of their confidence. This approach harnesses the predictive and data fusion capabilities of neural networks while also quantifying uncertainty. The results demonstrate that the multi-fidelity Bayesian model outperforms the state-of-the-art Co-Kriging in terms of overall accuracy and robustness on unseen data.
Paper Structure (10 sections, 4 equations, 4 figures, 3 tables, 1 algorithm)

This paper contains 10 sections, 4 equations, 4 figures, 3 tables, 1 algorithm.

Figures (4)

  • Figure 1: Architecture schema of MF-BayNet
  • Figure 2: Schematic of the half-span BSCW.
  • Figure 3: Design variable distribution (AoA-Mach) and aerodynamic coefficient predictions for each fidelity level.
  • Figure 4: Comparison of MF-BayNet and Co-Kriging predictions for $C_L$ and $C_M$ at two Mach numbers ($M=0.74$ and $M=0.82$) across varying AoA.