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디퓨저 깃배치각의 변화에 따른 원심압축기의 공력성능 특성에 관한 수치 연구

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dc.contributor.author박태규-
dc.contributor.author정인수-
dc.contributor.author정희택-
dc.contributor.author박준영-
dc.contributor.author김세미-
dc.contributor.author백제현-
dc.date.accessioned2022-12-27T04:36:45Z-
dc.date.available2022-12-27T04:36:45Z-
dc.date.issued2010-
dc.identifier.issn1598-6071-
dc.identifier.urihttps://scholarworks.gnu.ac.kr/handle/sw.gnu/25604-
dc.description.abstractIn the present study, the effects of the stagger angles on the aerodynamic performances in the vaned centrifugal compressor has been investigated by CFD methods. The diffuser vane angles were varied in the range of ±10 deg. from the initial-design points. The commercial Navier-Stokes solver, ANSYS-CFX were applied to solve the impeller-diffuser flowfields. Through the numerical results, the desirable setting angles were proposed to fit the best performance to the variation of the operating conditions.-
dc.format.extent6-
dc.language한국어-
dc.language.isoKOR-
dc.publisher한국전산유체공학회-
dc.title디퓨저 깃배치각의 변화에 따른 원심압축기의 공력성능 특성에 관한 수치 연구-
dc.title.alternativeNUMERICAL INVESTIGATION OF THE EFFECT OF THE STAGGER ANGLE ON THE AERODYNAMIC PERFORMANCES IN THE VANED DIFFUSER OF A CENTRIFUGAL COMPRESSOR-
dc.typeArticle-
dc.publisher.location대한민국-
dc.identifier.bibliographicCitation한국전산유체공학회지, v.15, no.3, pp 60 - 65-
dc.citation.title한국전산유체공학회지-
dc.citation.volume15-
dc.citation.number3-
dc.citation.startPage60-
dc.citation.endPage65-
dc.identifier.kciidART001482488-
dc.description.isOpenAccessN-
dc.description.journalRegisteredClasskci-
dc.subject.keywordAuthor공력성능(Aerodynamic Performance)-
dc.subject.keywordAuthor깃 배치각(Stagger Angle)-
dc.subject.keywordAuthor원심압축기(Centrifugal Compressor)-
dc.subject.keywordAuthor디퓨저(Diffuser)-
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공과대학 > Department of Mechanical Engineering > Journal Articles

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