초음속 충돌 제트 유동에 대한 k-w 난류모델의 적용Numerical Study on k-ω Turbulence Models for Supersonic Impinging Jet Flow Field

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dc.contributor.author김유진-
dc.contributor.author박수형-
dc.contributor.author권장혁-
dc.contributor.author김성인-
dc.contributor.author박승오-
dc.contributor.author이광섭-
dc.contributor.author홍승규-
dc.date.accessioned2013-03-18T19:53:17Z-
dc.date.available2013-03-18T19:53:17Z-
dc.date.created2012-02-06-
dc.date.issued2004-03-
dc.identifier.citation한국전산유체공학회 춘계학술대회, v., no., pp.139 - 145-
dc.identifier.urihttp://hdl.handle.net/10203/151902-
dc.description.abstractA numerical study of underexpanded jet and impingement on a wall mounted at various distances from the nozzle exit is presented. The 3-dimensional Navier-Stokes equations and k-ω turbulence equations are solved. The grids are constructed as overlapped grid systems to examine the distance effect. The DADI method is applied to obtain steady-state solutions. To avoid numerical instability such as the carbuncle that sometimes accompany approximate Riemann solver, the HLLE+ scheme is employed for the inviscid flux at the cell interfaces. A goal of this work is to apply a number of two-equation turbulence models based on the ω equation to the impinging jet problem.-
dc.languageKOR-
dc.publisher한국전산유체공학회-
dc.title초음속 충돌 제트 유동에 대한 k-w 난류모델의 적용-
dc.title.alternativeNumerical Study on k-ω Turbulence Models for Supersonic Impinging Jet Flow Field-
dc.typeConference-
dc.type.rimsCONF-
dc.citation.beginningpage139-
dc.citation.endingpage145-
dc.citation.publicationname한국전산유체공학회 춘계학술대회-
dc.identifier.conferencecountrySouth Korea-
dc.identifier.conferencecountrySouth Korea-
dc.contributor.localauthor권장혁-
dc.contributor.localauthor박승오-
dc.contributor.nonIdAuthor김유진-
dc.contributor.nonIdAuthor박수형-
dc.contributor.nonIdAuthor김성인-
dc.contributor.nonIdAuthor이광섭-
dc.contributor.nonIdAuthor홍승규-
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AE-Conference Papers(학술회의논문)AE-Conference Papers(학술회의논문)
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