Solution of Navier-Stokes equations by fourth-order compact schemes and AUSM flux splitting

Purpose - To develop a high-order compact finite-difference method for solving flow problems containing shock waves. Design/methodology/approach - A numerical algorithm based on high-order compact finite-difference schemes is developed for solving Navier-Stokes equations in two-dimensional space. Th...

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Main Authors: Mawlood M.K., Basri S., Asrar W., Omar A.A., Mokhtar A.S., Ahmad M.M.H.M.
Other Authors: 6507670187
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Published: 2023
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spelling my.uniten.dspace-297932023-12-28T16:57:42Z Solution of Navier-Stokes equations by fourth-order compact schemes and AUSM flux splitting Mawlood M.K. Basri S. Asrar W. Omar A.A. Mokhtar A.S. Ahmad M.M.H.M. 6507670187 6603349880 6603244837 7202864035 56186284800 7402896178 Finite difference methods Flow Wave properties finite difference technique heat flux mathematical analysis Navier-Stokes equations Algorithms Boundary layers Finite difference method Navier Stokes equations Shock waves Advection upstream splitting method (AUSM) Shear layers Wave properties Heat flux Purpose - To develop a high-order compact finite-difference method for solving flow problems containing shock waves. Design/methodology/approach - A numerical algorithm based on high-order compact finite-difference schemes is developed for solving Navier-Stokes equations in two-dimensional space. The convective flux terms are discretized by using advection upstream splitting method (AUSM). The developed method is then used to compute some example laminar flow problems. The problems considered have a range of Mach number that corresponds to subsonic incompressible flow to hypersonic compressible flows that contain shock waves and shock/boundary-layer interaction. Findings - The paper shows that the AUSM flux splitting and high-order compact finite-difference methods can be used accurately and robustly in resolving shear layers and capturing shock waves. The highly diffusive nature of conventional flux splitting especially on coarse grids makes them inaccurate for boundary layers even with high-order discretization. Originality/value - This paper presents a high-order numerical method that can accurately and robustly capture shock waves without deteriorating oscillations and resolve boundary layers and shock/boundary layer interaction. � Emerald Group Publishing Limited. Final 2023-12-28T08:57:42Z 2023-12-28T08:57:42Z 2006 Article 10.1108/09615530610636982 2-s2.0-30344459098 https://www.scopus.com/inward/record.uri?eid=2-s2.0-30344459098&doi=10.1108%2f09615530610636982&partnerID=40&md5=31d620ccb09538722e78e7c1343efe42 https://irepository.uniten.edu.my/handle/123456789/29793 16 1 107 120 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 Finite difference methods
Flow
Wave properties
finite difference technique
heat flux
mathematical analysis
Navier-Stokes equations
Algorithms
Boundary layers
Finite difference method
Navier Stokes equations
Shock waves
Advection upstream splitting method (AUSM)
Shear layers
Wave properties
Heat flux
spellingShingle Finite difference methods
Flow
Wave properties
finite difference technique
heat flux
mathematical analysis
Navier-Stokes equations
Algorithms
Boundary layers
Finite difference method
Navier Stokes equations
Shock waves
Advection upstream splitting method (AUSM)
Shear layers
Wave properties
Heat flux
Mawlood M.K.
Basri S.
Asrar W.
Omar A.A.
Mokhtar A.S.
Ahmad M.M.H.M.
Solution of Navier-Stokes equations by fourth-order compact schemes and AUSM flux splitting
description Purpose - To develop a high-order compact finite-difference method for solving flow problems containing shock waves. Design/methodology/approach - A numerical algorithm based on high-order compact finite-difference schemes is developed for solving Navier-Stokes equations in two-dimensional space. The convective flux terms are discretized by using advection upstream splitting method (AUSM). The developed method is then used to compute some example laminar flow problems. The problems considered have a range of Mach number that corresponds to subsonic incompressible flow to hypersonic compressible flows that contain shock waves and shock/boundary-layer interaction. Findings - The paper shows that the AUSM flux splitting and high-order compact finite-difference methods can be used accurately and robustly in resolving shear layers and capturing shock waves. The highly diffusive nature of conventional flux splitting especially on coarse grids makes them inaccurate for boundary layers even with high-order discretization. Originality/value - This paper presents a high-order numerical method that can accurately and robustly capture shock waves without deteriorating oscillations and resolve boundary layers and shock/boundary layer interaction. � Emerald Group Publishing Limited.
author2 6507670187
author_facet 6507670187
Mawlood M.K.
Basri S.
Asrar W.
Omar A.A.
Mokhtar A.S.
Ahmad M.M.H.M.
format Article
author Mawlood M.K.
Basri S.
Asrar W.
Omar A.A.
Mokhtar A.S.
Ahmad M.M.H.M.
author_sort Mawlood M.K.
title Solution of Navier-Stokes equations by fourth-order compact schemes and AUSM flux splitting
title_short Solution of Navier-Stokes equations by fourth-order compact schemes and AUSM flux splitting
title_full Solution of Navier-Stokes equations by fourth-order compact schemes and AUSM flux splitting
title_fullStr Solution of Navier-Stokes equations by fourth-order compact schemes and AUSM flux splitting
title_full_unstemmed Solution of Navier-Stokes equations by fourth-order compact schemes and AUSM flux splitting
title_sort solution of navier-stokes equations by fourth-order compact schemes and ausm flux splitting
publishDate 2023
_version_ 1806428378806353920
score 13.211869