Investigation of Numerical Dissipation in Classical and Implicit Large Eddy Simulations

The quantitative measure of dissipative properties of different numerical schemes is crucial to computational methods in the field of aerospace applications. Therefore, the objective of the present study is to examine the resolving power of Monotonic Upwind Scheme for Conservation Laws (MUSCL) schem...

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Main Authors: Moutassem El Rafei, László Könözsy, Zeeshan Rana
Format: Article
Language:English
Published: MDPI AG 2017-12-01
Series:Aerospace
Subjects:
Online Access:https://www.mdpi.com/2226-4310/4/4/59
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spelling doaj-578fdc51fef0432594635a08d8dad92b2020-11-25T01:49:20ZengMDPI AGAerospace2226-43102017-12-01445910.3390/aerospace4040059aerospace4040059Investigation of Numerical Dissipation in Classical and Implicit Large Eddy SimulationsMoutassem El Rafei0László Könözsy1Zeeshan Rana2Centre for Computational Engineering Sciences, Cranfield University, Cranfield, Bedfordshire MK43 0AL, UKCentre for Computational Engineering Sciences, Cranfield University, Cranfield, Bedfordshire MK43 0AL, UKCentre for Computational Engineering Sciences, Cranfield University, Cranfield, Bedfordshire MK43 0AL, UKThe quantitative measure of dissipative properties of different numerical schemes is crucial to computational methods in the field of aerospace applications. Therefore, the objective of the present study is to examine the resolving power of Monotonic Upwind Scheme for Conservation Laws (MUSCL) scheme with three different slope limiters: one second-order and two third-order used within the framework of Implicit Large Eddy Simulations (ILES). The performance of the dynamic Smagorinsky subgrid-scale model used in the classical Large Eddy Simulation (LES) approach is examined. The assessment of these schemes is of significant importance to understand the numerical dissipation that could affect the accuracy of the numerical solution. A modified equation analysis has been employed to the convective term of the fully-compressible Navier–Stokes equations to formulate an analytical expression of truncation error for the second-order upwind scheme. The contribution of second-order partial derivatives in the expression of truncation error showed that the effect of this numerical error could not be neglected compared to the total kinetic energy dissipation rate. Transitions from laminar to turbulent flow are visualized considering the inviscid Taylor–Green Vortex (TGV) test-case. The evolution in time of volumetrically-averaged kinetic energy and kinetic energy dissipation rate have been monitored for all numerical schemes and all grid levels. The dissipation mechanism has been compared to Direct Numerical Simulation (DNS) data found in the literature at different Reynolds numbers. We found that the resolving power and the symmetry breaking property are enhanced with finer grid resolutions. The production of vorticity has been observed in terms of enstrophy and effective viscosity. The instantaneous kinetic energy spectrum has been computed using a three-dimensional Fast Fourier Transform (FFT). All combinations of numerical methods produce a k − 4 spectrum at t * = 4 , and near the dissipation peak, all methods were capable of predicting the k − 5 / 3 slope accurately when refining the mesh.https://www.mdpi.com/2226-4310/4/4/59large eddy simulationTaylor–Green vortexnumerical dissipationmodified equation analysistruncation errorMUSCLdynamic Smagorinsky subgrid-scale modelkinetic energy dissipation
collection DOAJ
language English
format Article
sources DOAJ
author Moutassem El Rafei
László Könözsy
Zeeshan Rana
spellingShingle Moutassem El Rafei
László Könözsy
Zeeshan Rana
Investigation of Numerical Dissipation in Classical and Implicit Large Eddy Simulations
Aerospace
large eddy simulation
Taylor–Green vortex
numerical dissipation
modified equation analysis
truncation error
MUSCL
dynamic Smagorinsky subgrid-scale model
kinetic energy dissipation
author_facet Moutassem El Rafei
László Könözsy
Zeeshan Rana
author_sort Moutassem El Rafei
title Investigation of Numerical Dissipation in Classical and Implicit Large Eddy Simulations
title_short Investigation of Numerical Dissipation in Classical and Implicit Large Eddy Simulations
title_full Investigation of Numerical Dissipation in Classical and Implicit Large Eddy Simulations
title_fullStr Investigation of Numerical Dissipation in Classical and Implicit Large Eddy Simulations
title_full_unstemmed Investigation of Numerical Dissipation in Classical and Implicit Large Eddy Simulations
title_sort investigation of numerical dissipation in classical and implicit large eddy simulations
publisher MDPI AG
series Aerospace
issn 2226-4310
publishDate 2017-12-01
description The quantitative measure of dissipative properties of different numerical schemes is crucial to computational methods in the field of aerospace applications. Therefore, the objective of the present study is to examine the resolving power of Monotonic Upwind Scheme for Conservation Laws (MUSCL) scheme with three different slope limiters: one second-order and two third-order used within the framework of Implicit Large Eddy Simulations (ILES). The performance of the dynamic Smagorinsky subgrid-scale model used in the classical Large Eddy Simulation (LES) approach is examined. The assessment of these schemes is of significant importance to understand the numerical dissipation that could affect the accuracy of the numerical solution. A modified equation analysis has been employed to the convective term of the fully-compressible Navier–Stokes equations to formulate an analytical expression of truncation error for the second-order upwind scheme. The contribution of second-order partial derivatives in the expression of truncation error showed that the effect of this numerical error could not be neglected compared to the total kinetic energy dissipation rate. Transitions from laminar to turbulent flow are visualized considering the inviscid Taylor–Green Vortex (TGV) test-case. The evolution in time of volumetrically-averaged kinetic energy and kinetic energy dissipation rate have been monitored for all numerical schemes and all grid levels. The dissipation mechanism has been compared to Direct Numerical Simulation (DNS) data found in the literature at different Reynolds numbers. We found that the resolving power and the symmetry breaking property are enhanced with finer grid resolutions. The production of vorticity has been observed in terms of enstrophy and effective viscosity. The instantaneous kinetic energy spectrum has been computed using a three-dimensional Fast Fourier Transform (FFT). All combinations of numerical methods produce a k − 4 spectrum at t * = 4 , and near the dissipation peak, all methods were capable of predicting the k − 5 / 3 slope accurately when refining the mesh.
topic large eddy simulation
Taylor–Green vortex
numerical dissipation
modified equation analysis
truncation error
MUSCL
dynamic Smagorinsky subgrid-scale model
kinetic energy dissipation
url https://www.mdpi.com/2226-4310/4/4/59
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