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목적 공력특성 달성을 위한 플루트 노즐 전산설계

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dc.contributor.author강영진-
dc.contributor.author양영록-
dc.contributor.author황의창-
dc.contributor.author명노신-
dc.contributor.author조태환-
dc.date.accessioned2022-12-27T03:32:52Z-
dc.date.available2022-12-27T03:32:52Z-
dc.date.issued2011-
dc.identifier.issn1598-6071-
dc.identifier.urihttps://scholarworks.gnu.ac.kr/handle/sw.gnu/24252-
dc.description.abstractAs a preliminary design study to achieve target aerodynamic performance, this work was conducted on an original nozzle with 9 flutes in order to design a fluted nozzle with 12 flutes. The thrust and rolling moment of the nozzle with 12 flutes were analyzed using a CFD code according to the depth and rotation angle of the flutes. Based on this, a fluted nozzle with 12 flutes was optimized to yield the same thrust as that of the original nozzle with 9 flutes. The response surface method was applied for shape optimization of the fluted nozzle and design variables were selected to determine the depth angle and rotation angle of the flutes. An optimized shape that led to a thrust as strong as that of the original nozzle was obtained.-
dc.format.extent7-
dc.language한국어-
dc.language.isoKOR-
dc.publisher한국전산유체공학회-
dc.title목적 공력특성 달성을 위한 플루트 노즐 전산설계-
dc.title.alternativeCOMPUTATIONAL DESIGN OF A FLUTED NOZZLE FOR ACHIEVING TARGET AERODYNAMIC PERFORMANCE-
dc.typeArticle-
dc.publisher.location대한민국-
dc.identifier.bibliographicCitation한국전산유체공학회지, v.16, no.3, pp 1 - 7-
dc.citation.title한국전산유체공학회지-
dc.citation.volume16-
dc.citation.number3-
dc.citation.startPage1-
dc.citation.endPage7-
dc.identifier.kciidART001588920-
dc.description.isOpenAccessN-
dc.description.journalRegisteredClasskci-
dc.subject.keywordAuthor로켓 노즐 설계(Rocket Nozzle Design)-
dc.subject.keywordAuthor플루트 노즐(Fluted Nozzle)-
dc.subject.keywordAuthor노즐 형상 최적화(Nozzle Shape Optimization)-
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공학계열 > 기계항공우주공학부 > Journal Articles

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