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An AUSM-based high-order compact method for solving Navier-Stokes equations

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dc.citedby1
dc.contributor.authorMawlood M.K.en_US
dc.contributor.authorBasri S.N.en_US
dc.contributor.authorAsrar W.en_US
dc.contributor.authorOmar A.A.en_US
dc.contributor.authorMokhtar A.S.en_US
dc.contributor.authorAhmad M.M.H.M.en_US
dc.contributor.authorid6507670187en_US
dc.contributor.authorid6603349880en_US
dc.contributor.authorid6603244837en_US
dc.contributor.authorid7202864035en_US
dc.contributor.authorid56186284800en_US
dc.contributor.authorid7402896178en_US
dc.date.accessioned2023-12-28T08:57:58Z
dc.date.available2023-12-28T08:57:58Z
dc.date.issued2004
dc.description.abstractA high-order compact upwind algorithm is developed for solving Navier-Stokes equations in two-space dimensions. The method is based on advection upstream splitting method and fourth-order compact finite-difference schemes. The convection flux terms of the Navier-Stokes equations are discretized by a compact cell-centered differencing scheme while the diffusion flux terms are discretized by a central fourth-order compact scheme. The midpoint values of the flux functions required by the cell-centered compact scheme are determined by a fourth-order MUSCL approach. For steady-state solutions; first-order implicit time integration, with LU decomposition, is employed. Computed results for a laminar flow past a flat plate and the problem of shock-wave boundary layer interaction are presented.en_US
dc.description.natureFinalen_US
dc.identifier.doi10.1108/00022660410536032
dc.identifier.epage304
dc.identifier.issue3
dc.identifier.scopus2-s2.0-2542540557
dc.identifier.spage299
dc.identifier.urihttps://www.scopus.com/inward/record.uri?eid=2-s2.0-2542540557&doi=10.1108%2f00022660410536032&partnerID=40&md5=60b557cbc9bb364949451ed95c418df9
dc.identifier.urihttps://irepository.uniten.edu.my/handle/123456789/29857
dc.identifier.volume76
dc.pagecount5
dc.sourceScopus
dc.sourcetitleAircraft Engineering and Aerospace Technology
dc.subjectDifferential equations
dc.subjectDynamics
dc.subjectGases
dc.subjectAlgorithms
dc.subjectBoundary layers
dc.subjectFinite difference method
dc.subjectFunctions
dc.subjectLaminar flow
dc.subjectNavier Stokes equations
dc.subjectShock waves
dc.subjectTwo dimensional
dc.subjectHigh order compact unwind algorithm
dc.subjectTwo space dimensions
dc.subjectAerospace engineering
dc.titleAn AUSM-based high-order compact method for solving Navier-Stokes equationsen_US
dc.typeArticleen_US
dspace.entity.typePublication
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