Machine learning based uncertainty quantification of turbulence model for airfoils
Minghan Chu, Weicheng Qian

TL;DR
This paper introduces lightweight machine learning models, polynomial regression and CNN, to improve the estimation of RANS model uncertainties in airflow over airfoils, enhancing turbulence transition predictions.
Contribution
It presents novel, simple machine learning approaches to select perturbation strength in eigenspace perturbation, improving RANS uncertainty quantification for airfoil flows.
Findings
Lightweight models effectively estimate turbulence kinetic energy.
Models improve the accuracy of RANS uncertainty bounds.
CNN-based marker function enhances turbulence transition modeling.
Abstract
Reynolds-averaged Navier-Stokes (RANS)-based transition modeling is widely used in aerospace applications but suffers inaccuracies due to the Boussinesq turbulent viscosity hypothesis. The eigenspace perturbation method can estimate the accuracy of a RANS model by injecting perturbations to its predicted Reynolds stresses. However, there lacks a reliable method for choosing the strength of the injected perturbation, while existing machine learning models are often complex and data craving. We examined two light-weighted machine learning models to help select the strength of the injected perturbation for estimating the RANS uncertainty of flows undergoing the transition to turbulence over a Selig-Donovan 7003 airfoil. On the one hand, we examined polynomial regression to construct a marker function augmented with eigenvalue perturbations to estimate the uncertainty bound for the…
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Taxonomy
TopicsModel Reduction and Neural Networks · Fluid Dynamics and Turbulent Flows · Aerodynamics and Acoustics in Jet Flows
