On the accuracy of eddy-viscosity and eddy-conductivity models in square duct flow
ORAL
Abstract
We carry out a priori tests of linear and nonlinear eddy-viscosity models using direct numerical simulation (DNS) data of square duct flow up to friction Reynolds number Reτ = 2000. We focus on the ability of eddy-viscosity models to reproduce the anisotropic Reynolds stress tensor components aij responsible for turbulent secondary flows, namely the normal stress a22 and the secondary shear stress a23. We perform two types of tests: i) on constitutive relations and ii) on RANS models. A priori tests on constitutive relations for aij are performed using the tensor polynomial expansion of Pope, and they allow us to assess the maximum accuracy that one can achieve for different orders of the tensor polynomial, where one tensor base corresponds to the linear eddy-viscosity hypothesis and five bases return the exact representation of aij. Models performance are quantified using the mean correlation coefficient with respect to DNS data Cij, which shows that the linear eddy-viscosity hypothesis always returns very accurate values of the primary shear stress (C12>0.99), whereas two bases are sufficient to achieve good accuracy of the normal stress and secondary shear stress (C22=0.911, C23=0.743). Instead, a priori analysis carried out on popular RANS models, including k–ε and v2–f, reveals that none of them achieves ideal accuracy. The only model which approaches ideal performance is the quadratic correction of Spalart, which has an accuracy similar to models using four or more tensor bases. An equivalent approach, based on vector integrity bases, is used to assess the accuracy of eddy-conductivity models for approximating the turbulent-heat flux.
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Publication: Modesti, D. "A priori tests of eddy viscosity models in square duct flow." Theoretical and Computational Fluid Dynamics 34.5 (2020): 713-734.
Presenters
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Davide Modesti
Faculty of Aerospace Engineering, Delft University of Technology, HS Delft, The Netherlands, Delft University of Technology
Authors
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Davide Modesti
Faculty of Aerospace Engineering, Delft University of Technology, HS Delft, The Netherlands, Delft University of Technology