포텐셜 패널과 와류 조각 연계방법을 이용한 로터 공력 해석 Potential Panel and Vortex Particle Coupling Analysis

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dc.contributor.author장지성ko
dc.contributor.author정인재ko
dc.contributor.author이덕주ko
dc.date.accessioned2015-11-20T12:35:32Z-
dc.date.available2015-11-20T12:35:32Z-
dc.date.created2014-01-15-
dc.date.created2014-01-15-
dc.date.issued2013-08-
dc.identifier.citation한국군사과학기술학회지, v.16, no.4, pp.481 - 485-
dc.identifier.issn1598-9127-
dc.identifier.urihttp://hdl.handle.net/10203/201573-
dc.description.abstractRotor wake causes unsteady aerodynamics of rotor blade. So, accurate prediction of wake is very important and vortex method is good solution for this problem. Aerodynamic force of the rotor blade is calculated by potential panel method and the rotor wake is simulated by vortex particle method. The vortex particle method is easier to treat wake-body interaction and has better performance to expect the effect of ground and fuselage interaction. Rotor in hovering and forward flight condition is simulated through these methods. Thrust and surface pressure of rotor are compared with experiment data.-
dc.languageKorean-
dc.publisher한국군사과학기술학회-
dc.title포텐셜 패널과 와류 조각 연계방법을 이용한 로터 공력 해석-
dc.title.alternativePotential Panel and Vortex Particle Coupling Analysis-
dc.typeArticle-
dc.type.rimsART-
dc.citation.volume16-
dc.citation.issue4-
dc.citation.beginningpage481-
dc.citation.endingpage485-
dc.citation.publicationname한국군사과학기술학회지-
dc.identifier.kciidART001798797-
dc.contributor.localauthor이덕주-
dc.contributor.nonIdAuthor장지성-
dc.contributor.nonIdAuthor정인재-
dc.subject.keywordAuthorRotor(회전날개)-
dc.subject.keywordAuthorVortex method(와류방법)-
dc.subject.keywordAuthorAerodynamics(공기역학)-
Appears in Collection
AE-Journal Papers(저널논문)
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