큰 깃배치각을 갖는 천음속 압축기 정익-동익 段유동에 관한 복합격자의 해Composite-Grid Solution to the Transonic Compressor Stator-Rotor Stage Flow at High Stagger Angle

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dc.contributor.author강인모ko
dc.contributor.author장근식ko
dc.date.accessioned2013-02-25T02:18:12Z-
dc.date.available2013-02-25T02:18:12Z-
dc.date.created2012-02-06-
dc.date.created2012-02-06-
dc.date.issued1994-04-
dc.identifier.citation한국항공우주학회지, v.22, no.2, pp.36 - 45-
dc.identifier.issn1225-1348-
dc.identifier.urihttp://hdl.handle.net/10203/59048-
dc.languageEnglish-
dc.publisher한국항공우주학회-
dc.title큰 깃배치각을 갖는 천음속 압축기 정익-동익 段유동에 관한 복합격자의 해-
dc.title.alternativeComposite-Grid Solution to the Transonic Compressor Stator-Rotor Stage Flow at High Stagger Angle-
dc.typeArticle-
dc.type.rimsART-
dc.citation.volume22-
dc.citation.issue2-
dc.citation.beginningpage36-
dc.citation.endingpage45-
dc.citation.publicationname한국항공우주학회지-
dc.contributor.localauthor장근식-
dc.contributor.nonIdAuthor강인모-
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