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Waterjet Intake 유도관 성능시험시스템 개발

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dc.contributor.author안종우-
dc.contributor.author박영하-
dc.contributor.author김기섭-
dc.contributor.author김경열-
dc.date.accessioned2021-12-09T01:40:34Z-
dc.date.available2021-12-09T01:40:34Z-
dc.date.issued20021211-
dc.identifier.urihttps://www.kriso.re.kr/sciwatch/handle/2021.sw.kriso/7371-
dc.description.abstractIn order to develope the intake-diffuser with good performance for the waterjet propulsion system, new experimental device was designed and manufactured. The experimental device is installed on the test section of the KRISO cavitation tunnel. The efficiency of the intake-diffuser is calculated using the measurement result of 1-hole and 5-hole pitot tubes(probes). The calibration of the 5-hole probes is conducted at the cavitation tunnel. The cavitation inception occurs at the intake lip, and its occurrence location depends on IVR (Inlet Velocity Ratio) condition.-
dc.language영어-
dc.language.isoENG-
dc.titleWaterjet Intake 유도관 성능시험시스템 개발-
dc.title.alternativeDevelopment of performance test system for waterjet Intake-diffuser-
dc.typeConference-
dc.citation.titleThe 2nd PNU International Colloquim on Waterjet-
dc.citation.conferenceNameThe 2nd PNU International Colloquim on Waterjet-
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선박연구본부 > Naval Ship Engineering Research Center > 2. Conference Papers

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지능형선박연구본부 (함정공학연구센터)
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