DC Field | Value | Language |
---|---|---|
dc.contributor.author | 김주성 | ko |
dc.contributor.author | 강희정 | ko |
dc.contributor.author | 박영민 | ko |
dc.contributor.author | 권오준 | ko |
dc.date.accessioned | 2013-02-28T02:12:03Z | - |
dc.date.available | 2013-02-28T02:12:03Z | - |
dc.date.created | 2012-02-06 | - |
dc.date.created | 2012-02-06 | - |
dc.date.issued | 2000-09 | - |
dc.identifier.citation | 한국전산유체공학회지, v.5, no.2, pp.20 - 27 | - |
dc.identifier.issn | 1598-6071 | - |
dc.identifier.uri | http://hdl.handle.net/10203/72222 | - |
dc.description.abstract | An unstructured implicit Euler solver is parallelized on a Cray T3E. Spatial discretization is accomplished by a cell-centered finite volume formulation using an upwind flux differencing. Time is advanced by the Gauss-Seidel implicit scheme. Domain decomposition is accomplished by using the k-way n-partitioning method developed by Karypis. In order to analyze the parallel performance of the solver, flows over a 2-D NACA 0012 airfoil and 3-D F-5 wing were investigated. | - |
dc.language | Korean | - |
dc.publisher | 한국전산유체공학회 | - |
dc.title | 내재적 방법을 이용한 비정렬 유동해석 기법의 병렬화 | - |
dc.title.alternative | Parallelization of an Unstructured Implicit Euler Solver | - |
dc.type | Article | - |
dc.type.rims | ART | - |
dc.citation.volume | 5 | - |
dc.citation.issue | 2 | - |
dc.citation.beginningpage | 20 | - |
dc.citation.endingpage | 27 | - |
dc.citation.publicationname | 한국전산유체공학회지 | - |
dc.contributor.localauthor | 권오준 | - |
dc.contributor.nonIdAuthor | 김주성 | - |
dc.contributor.nonIdAuthor | 강희정 | - |
dc.contributor.nonIdAuthor | 박영민 | - |
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