DC Field | Value | Language |
---|---|---|
dc.contributor.author | 김민환 | ko |
dc.contributor.author | 박승오 | ko |
dc.date.accessioned | 2009-12-09T01:42:31Z | - |
dc.date.available | 2009-12-09T01:42:31Z | - |
dc.date.created | 2012-02-06 | - |
dc.date.created | 2012-02-06 | - |
dc.date.issued | 1998-05 | - |
dc.identifier.citation | 한국항공우주학회지, v.26, no.3, pp.36 - 44 | - |
dc.identifier.issn | 1225-1348 | - |
dc.identifier.uri | http://hdl.handle.net/10203/14408 | - |
dc.description.abstract | The performance of one-equation turbulence models of Baldwin-Barth and Spalart-Allmaras is assessed against shock-turbulent boundary layer interaction flow. The flow configurations are the 20 degree compression ramp flow and the axisymmetric bump flow. The Baldwin-Lomax, Baldwin-Barth, and Spalart-Allmaras models have been implemented into the compressible Navier-Stokdes code. Modification of the Baldwin-Barth model for non-equilibrium turbulence flow is suggested. Computational results indicate that the model modification yielded substantially improved solution. | - |
dc.language | Korean | - |
dc.language.iso | ko | en |
dc.publisher | 한국항공우주학회 | - |
dc.title | 1-방정식 모형을 이용한 충격파-난류 경계층 상호작용 유동의 해석 | - |
dc.title.alternative | Computation of Shock-Turbulent Boundary Layer Interaction Flow with One-Equation Turbulence Models | - |
dc.type | Article | - |
dc.publisher.alternative | The Korean Society for Aeronautical & Space Sciences | en |
dc.type.rims | ART | - |
dc.citation.volume | 26 | - |
dc.citation.issue | 3 | - |
dc.citation.beginningpage | 36 | - |
dc.citation.endingpage | 44 | - |
dc.citation.publicationname | 한국항공우주학회지 | - |
dc.embargo.liftdate | 9999-12-31 | - |
dc.embargo.terms | 9999-12-31 | - |
dc.contributor.localauthor | 박승오 | - |
dc.contributor.nonIdAuthor | 김민환 | - |
Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.