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터보차져에서 터빈 노즐각에 따른 컴프레서 압축비 예측

DC Field Value Language
dc.contributor.advisor송성진-
dc.contributor.author정왕조-
dc.date.accessioned2010-01-26T03:51:42Z-
dc.date.available2010-01-26T03:51:42Z-
dc.date.copyright2004.-
dc.date.issued2004-
dc.identifier.urihttp://dcollection.snu.ac.kr:80/jsp/common/DcLoOrgPer.jsp?sItemId=000000056619kog
dc.identifier.urihttps://hdl.handle.net/10371/44462-
dc.description학위논문(석사)--서울대학교 대학원 :기계항공공학부,2004.ko
dc.format.extentv, 31 장ko
dc.language.isokoko
dc.publisher서울대학교 대학원ko
dc.subject터보차져ko
dc.subjectTurbochargerko
dc.subject가변 노즐ko
dc.subjectVariable Nozzleko
dc.subject컴프레서 압축비ko
dc.subjectCompressor Pressure Ratioko
dc.title터보차져에서 터빈 노즐각에 따른 컴프레서 압축비 예측ko
dc.typeThesis-
dc.contributor.department기계항공공학부-
dc.description.degreeMasterko
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