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Cited 6 time in webofscience Cited 8 time in scopus
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dc.contributor.authorInho Kim-
dc.contributor.authorLee, JW-
dc.contributor.authorChoi, MK-
dc.contributor.authorS.J. Kwon-
dc.date.accessioned2016-03-31T09:10:34Z-
dc.date.available2016-03-31T09:10:34Z-
dc.date.created2012-03-19-
dc.date.issued2011-08-
dc.identifier.issn1556-7265-
dc.identifier.other2011-OAK-0000024918-
dc.identifier.urihttps://oasis.postech.ac.kr/handle/2014.oak/16765-
dc.description.abstractThe characteristics of supersonic flow field and thrust for a micronozzle used in a microthruster were analyzed numerically to determine the optimum nozzle geometry. Typical parameter values are 300 mu m throat diameter, 10 bar and 1000 K for stagnation conditions, and 1-100 ms for combustion completion. The effects of the boundary layer, heat loss, and unsteady stagnation conditions were considered. Thrust was much more dependent on the nozzle expansion angle than the area ratio or length. Optimum nozzle expansion angle for maximum thrust was close to 30 degrees for a planar 2D nozzle and 25 degrees for a 2D axisymmetric nozzle.-
dc.description.statementofresponsibilityX-
dc.languageEnglish-
dc.publisherTaylor and Francis-
dc.relation.isPartOfNANOSCALE AND MICROSCALE THERMOPHYSICAL ENGINEERING-
dc.subjectmicro solid-propellant thruster-
dc.subjectmicronozzle-
dc.subjectoptimum angle-
dc.subjectSPRAY PROCESS-
dc.subjectPERFORMANCE-
dc.titleOptimum Nozzle Angle of a Micro Solid-propellant Thruster-
dc.typeArticle-
dc.contributor.college기계공학과-
dc.identifier.doi10.1080/15567265.2011.597491-
dc.author.googleKim, I-
dc.author.googleLee, JW-
dc.author.googleChoi, MK-
dc.author.googleKwon, S-
dc.relation.volume15-
dc.relation.issue3-
dc.relation.startpage165-
dc.relation.lastpage178-
dc.contributor.id10069926-
dc.relation.journalNANOSCALE AND MICROSCALE THERMOPHYSICAL ENGINEERING-
dc.relation.indexSCI급, SCOPUS 등재논문-
dc.relation.sciSCI-
dc.collections.nameJournal Papers-
dc.type.rimsART-
dc.identifier.bibliographicCitationNANOSCALE AND MICROSCALE THERMOPHYSICAL ENGINEERING, v.15, no.3, pp.165 - 178-
dc.identifier.wosid000299472400003-
dc.date.tcdate2019-01-01-
dc.citation.endPage178-
dc.citation.number3-
dc.citation.startPage165-
dc.citation.titleNANOSCALE AND MICROSCALE THERMOPHYSICAL ENGINEERING-
dc.citation.volume15-
dc.contributor.affiliatedAuthorLee, JW-
dc.identifier.scopusid2-s2.0-80051537008-
dc.description.journalClass1-
dc.description.journalClass1-
dc.description.wostc4-
dc.description.scptc5*
dc.date.scptcdate2018-05-121*
dc.type.docTypeArticle-
dc.subject.keywordAuthormicro solid-propellant thruster-
dc.subject.keywordAuthormicronozzle-
dc.subject.keywordAuthoroptimum angle-
dc.relation.journalWebOfScienceCategoryThermodynamics-
dc.relation.journalWebOfScienceCategoryEngineering, Mechanical-
dc.relation.journalWebOfScienceCategoryNanoscience & Nanotechnology-
dc.relation.journalWebOfScienceCategoryMaterials Science, Characterization & Testing-
dc.relation.journalWebOfScienceCategoryPhysics, Applied-
dc.description.journalRegisteredClassscie-
dc.description.journalRegisteredClassscopus-
dc.relation.journalResearchAreaThermodynamics-
dc.relation.journalResearchAreaEngineering-
dc.relation.journalResearchAreaScience & Technology - Other Topics-
dc.relation.journalResearchAreaMaterials Science-
dc.relation.journalResearchAreaPhysics-

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이진원LEE, JIN WON
Dept of Mechanical Enginrg
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