High-order projection-based upwind method for simulation of transitional turbulent flows

Fuente: arXiv
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Main Authors: Lederer, Philip L., Mooslechner, Xaver, Schöberl, Joachim
Format: Preprint
Published: 2024
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author Lederer, Philip L.
Mooslechner, Xaver
Schöberl, Joachim
author_facet Lederer, Philip L.
Mooslechner, Xaver
Schöberl, Joachim
contents We present a scalable, high-order implicit large-eddy simulation (ILES) approach for incompressible transitional flows. This method employs the mass-conserving mixed stress (MCS) method for discretizing the Navier-Stokes equations. The MCS method's low dissipation characteristics, combined with the introduced operator-splitting solution technique, result in a high-order solver optimized for efficient and parallel computation of under-resolved turbulent flows. We further enhance the inherent capabilities of the ILES model by incorporating high-order upwind fluxes and are examining its approximation behaviour in transitional aerodynamic flow problems. In this study, we use flows over the Eppler 387 airfoil at Reynolds numbers up to $3 \cdot 10^5$ as benchmarks for our simulations.
format Preprint
id arxiv_https___arxiv_org_abs_2408_06698
institution arXiv
publishDate 2024
record_format arxiv
spellingShingle High-order projection-based upwind method for simulation of transitional turbulent flows
Lederer, Philip L.
Mooslechner, Xaver
Schöberl, Joachim
Computational Engineering, Finance, and Science
We present a scalable, high-order implicit large-eddy simulation (ILES) approach for incompressible transitional flows. This method employs the mass-conserving mixed stress (MCS) method for discretizing the Navier-Stokes equations. The MCS method's low dissipation characteristics, combined with the introduced operator-splitting solution technique, result in a high-order solver optimized for efficient and parallel computation of under-resolved turbulent flows. We further enhance the inherent capabilities of the ILES model by incorporating high-order upwind fluxes and are examining its approximation behaviour in transitional aerodynamic flow problems. In this study, we use flows over the Eppler 387 airfoil at Reynolds numbers up to $3 \cdot 10^5$ as benchmarks for our simulations.
title High-order projection-based upwind method for simulation of transitional turbulent flows
topic Computational Engineering, Finance, and Science
url https://arxiv.org/abs/2408.06698