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가스터빈 프리스월 시스템의 외기 온도와 터빈 부하 조건에 따른 탈설계점 특성 분석

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dc.contributor.authorPark, Hyunwoo-
dc.contributor.authorLee, Jungsoo-
dc.contributor.authorCho, Geonhwan-
dc.contributor.authorCho, Jinsoo-
dc.date.accessioned2021-08-02T10:27:48Z-
dc.date.available2021-08-02T10:27:48Z-
dc.date.created2021-05-12-
dc.date.issued2019-12-
dc.identifier.issn1225-1348-
dc.identifier.urihttps://scholarworks.bwise.kr/hanyang/handle/2021.sw.hanyang/11586-
dc.description.abstractThe pre-swirl system is the device that minimizes energy loss of turbine cooling airflow from the stationary parts into rotating parts. In this paper, an off-design analysis was conducted for the ambient air temperature and turbine load conditions. The discharge coefficient was constant for ambient air temperature and turbine load. However, adiabatic effectiveness was increased. This is due to the volume flow rate. The volume flow rate was increased at higher ambient temperature and higher turbine load. It means that the volume of cooling air was increased and the cooling performance of the air was improved. Consequently, adiabatic effectiveness increased by 30.46% at 100% turbine load compared to 20% turbine load. And increased by 18.42% at 55 degrees C ambient air temperature compared to -20 degrees C ambient air temperature.-
dc.language한국어-
dc.language.isoko-
dc.publisherKOREAN SOC AERONAUTICAL & SPACE SCIENCES-
dc.title가스터빈 프리스월 시스템의 외기 온도와 터빈 부하 조건에 따른 탈설계점 특성 분석-
dc.title.alternativeOff-design Characteristics for Ambient Air Temperature and Turbine Load of Gas Turbine Pre-swirl System-
dc.typeArticle-
dc.contributor.affiliatedAuthorCho, Jinsoo-
dc.identifier.doi10.5139/JKSAS.2019.47.12.881-
dc.identifier.scopusid2-s2.0-85150432793-
dc.identifier.wosid000537739000007-
dc.identifier.bibliographicCitationJOURNAL OF THE KOREAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, v.47, no.12, pp.881 - 889-
dc.relation.isPartOfJOURNAL OF THE KOREAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES-
dc.citation.titleJOURNAL OF THE KOREAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES-
dc.citation.volume47-
dc.citation.number12-
dc.citation.startPage881-
dc.citation.endPage889-
dc.type.rimsART-
dc.type.docTypeArticle-
dc.identifier.kciidART002529202-
dc.description.journalClass2-
dc.description.isOpenAccessN-
dc.description.journalRegisteredClasskci-
dc.relation.journalResearchAreaEngineering-
dc.relation.journalWebOfScienceCategoryEngineering, Aerospace-
dc.subject.keywordPlusFLOW-
dc.subject.keywordAuthorAmbient Air Temperature-
dc.subject.keywordAuthorGas Turbine-
dc.subject.keywordAuthorOff-design-
dc.subject.keywordAuthorPre-swirl System-
dc.subject.keywordAuthorSecondary Air System-
dc.subject.keywordAuthorTurbine Load-
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