3차원 비정렬 격자를 사용한 비점성 유동해석ulation of Inviscid Flows Using Three-Dimensional Unstructured Meshes
| DC Field | Value | Language |
|---|---|---|
| dc.contributor.author | 권오준 | ko |
| dc.date.accessioned | 2013-03-03T00:04:42Z | - |
| dc.date.available | 2013-03-03T00:04:42Z | - |
| dc.date.created | 2012-02-06 | - |
| dc.date.created | 2012-02-06 | - |
| dc.date.issued | 1996-02 | - |
| dc.identifier.citation | 한국항공우주학회지, v.24, no.1, pp.46 - 56 | - |
| dc.identifier.issn | 1225-1348 | - |
| dc.identifier.uri | http://hdl.handle.net/10203/76164 | - |
| dc.description.abstract | Inviscid compressible flows over wings and wing-body configurations are calculated using three-dimensional unstructured tetrahedral meshes. The equations are integrated in time with an explicit Runge-Kutta time-stepping algorithm. The inviscid flux terms are discretized based on a cell-centered finite-volume formulation with the Roe``e flux-difference splitting. The tetrahedral meshes are generated using an advancing-front technique. Good agreement is obtained between the present calculation and the experiment for both subsonic and transonic flight regimes. | - |
| dc.language | Korean | - |
| dc.publisher | 한국항공우주학회 | - |
| dc.title | 3차원 비정렬 격자를 사용한 비점성 유동해석 | - |
| dc.title.alternative | ulation of Inviscid Flows Using Three-Dimensional Unstructured Meshes | - |
| dc.type | Article | - |
| dc.type.rims | ART | - |
| dc.citation.volume | 24 | - |
| dc.citation.issue | 1 | - |
| dc.citation.beginningpage | 46 | - |
| dc.citation.endingpage | 56 | - |
| dc.citation.publicationname | 한국항공우주학회지 | - |
| dc.contributor.localauthor | 권오준 | - |
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