선회기 및 공연비 변화에 따른 모델연소기 선회유동장의 유동/분무 특성Flow and Spray Characteristics under Swirl Flow Field of a Model Combustor through Variation of Swirler and Air/Fuel Ratio

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dc.contributor.author이동훈-
dc.contributor.author박승훈-
dc.contributor.author배충식-
dc.date.accessioned2009-12-22T03:07:57Z-
dc.date.available2009-12-22T03:07:57Z-
dc.date.created2012-02-06-
dc.date.issued1998-11-
dc.identifier.citation한국항공우주학회 1998년 추계학술발표회, v., no., pp.200 - 206-
dc.identifier.urihttp://hdl.handle.net/10203/15560-
dc.languageKOR-
dc.language.isokoen
dc.publisher한국항고우주학회-
dc.title선회기 및 공연비 변화에 따른 모델연소기 선회유동장의 유동/분무 특성-
dc.title.alternativeFlow and Spray Characteristics under Swirl Flow Field of a Model Combustor through Variation of Swirler and Air/Fuel Ratio-
dc.typeConference-
dc.type.rimsCONF-
dc.citation.beginningpage200-
dc.citation.endingpage206-
dc.citation.publicationname한국항공우주학회 1998년 추계학술발표회-
dc.identifier.conferencecountrySouth Korea-
dc.identifier.conferencecountrySouth Korea-
dc.contributor.localauthor배충식-
dc.contributor.nonIdAuthor이동훈-
dc.contributor.nonIdAuthor박승훈-

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