Aerodynamic Data Fusion Towards the Digital Twin Paradigm
S. Ashwin Renganathan, Kohei Harada, Dimitri N. Mavris

TL;DR
This paper presents a Bayesian data fusion framework and a constrained POD method to combine different aerodynamic data sources, improving the estimation of true flow fields for aerospace design, especially under data scarcity.
Contribution
It introduces a Bayesian approach and an extended POD method for fusing multi-fidelity aerodynamic data, addressing uncertainties and biases in the data sources.
Findings
Bayesian method is more robust with scarce data.
Both methods yield similar results with sufficient data.
Fused data enhances surrogate model accuracy.
Abstract
We consider the fusion of two aerodynamic data sets originating from differing fidelity physical or computer experiments. We specifically address the fusion of: 1) noisy and in-complete fields from wind tunnel measurements and 2) deterministic but biased fields from numerical simulations. These two data sources are fused in order to estimate the \emph{true} field that best matches measured quantities that serves as the ground truth. For example, two sources of pressure fields about an aircraft are fused based on measured forces and moments from a wind-tunnel experiment. A fundamental challenge in this problem is that the true field is unknown and can not be estimated with 100\% certainty. We employ a Bayesian framework to infer the true fields conditioned on measured quantities of interest; essentially we perform a \emph{statistical correction} to the data. The fused data may then be…
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