Flux limiting with high-order compact schemes

In this paper, we present a modified flux limiter for limiting the numerical flux differences obtained from a fifth-order upwind compact scheme. The accuracy of the scheme is tested through the solution of the scalar 1D inviscid Burgers equation. The method is then used for solving the 2D Euler equa...

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Main Authors: Mawlood M.K., Basri S., Mokhtar A.S., Ahmad M.M.H.M., Asrar W., Omar A.A.
Other Authors: 6507670187
Format: Conference paper
Published: 2023
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spelling my.uniten.dspace-299112023-12-28T16:58:12Z Flux limiting with high-order compact schemes Mawlood M.K. Basri S. Mokhtar A.S. Ahmad M.M.H.M. Asrar W. Omar A.A. 6507670187 6603349880 56186284800 7402896178 6603244837 7202864035 Integration Oscillations Problem solving Runge Kutta methods Steady flow Unsteady flow Burgers equation Compact schemes Numerical flux Steady-state solutions Flow of fluids In this paper, we present a modified flux limiter for limiting the numerical flux differences obtained from a fifth-order upwind compact scheme. The accuracy of the scheme is tested through the solution of the scalar 1D inviscid Burgers equation. The method is then used for solving the 2D Euler equations for flows containing shocks. For unsteady problems, a multistage SSP Runge-Kutta method is employed for the time integration. For two-dimensional steady-state solutions, first-order implicit time integration, with LU decomposition, is employed. Results have shown that the developed flux limiter significantly eliminates the numerical oscillations. Copyright � 2005 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved. Final 2023-12-28T08:58:12Z 2023-12-28T08:58:12Z 2005 Conference paper 2-s2.0-30744470647 https://www.scopus.com/inward/record.uri?eid=2-s2.0-30744470647&partnerID=40&md5=5abba86369344b166d29e7f104b77033 https://irepository.uniten.edu.my/handle/123456789/29911 7637 7645 Scopus
institution Universiti Tenaga Nasional
building UNITEN Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider Universiti Tenaga Nasional
content_source UNITEN Institutional Repository
url_provider http://dspace.uniten.edu.my/
topic Integration
Oscillations
Problem solving
Runge Kutta methods
Steady flow
Unsteady flow
Burgers equation
Compact schemes
Numerical flux
Steady-state solutions
Flow of fluids
spellingShingle Integration
Oscillations
Problem solving
Runge Kutta methods
Steady flow
Unsteady flow
Burgers equation
Compact schemes
Numerical flux
Steady-state solutions
Flow of fluids
Mawlood M.K.
Basri S.
Mokhtar A.S.
Ahmad M.M.H.M.
Asrar W.
Omar A.A.
Flux limiting with high-order compact schemes
description In this paper, we present a modified flux limiter for limiting the numerical flux differences obtained from a fifth-order upwind compact scheme. The accuracy of the scheme is tested through the solution of the scalar 1D inviscid Burgers equation. The method is then used for solving the 2D Euler equations for flows containing shocks. For unsteady problems, a multistage SSP Runge-Kutta method is employed for the time integration. For two-dimensional steady-state solutions, first-order implicit time integration, with LU decomposition, is employed. Results have shown that the developed flux limiter significantly eliminates the numerical oscillations. Copyright � 2005 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.
author2 6507670187
author_facet 6507670187
Mawlood M.K.
Basri S.
Mokhtar A.S.
Ahmad M.M.H.M.
Asrar W.
Omar A.A.
format Conference paper
author Mawlood M.K.
Basri S.
Mokhtar A.S.
Ahmad M.M.H.M.
Asrar W.
Omar A.A.
author_sort Mawlood M.K.
title Flux limiting with high-order compact schemes
title_short Flux limiting with high-order compact schemes
title_full Flux limiting with high-order compact schemes
title_fullStr Flux limiting with high-order compact schemes
title_full_unstemmed Flux limiting with high-order compact schemes
title_sort flux limiting with high-order compact schemes
publishDate 2023
_version_ 1806424477599268864
score 13.214268