DC Field | Value | Language |
---|---|---|
dc.contributor.author | 장지성 | ko |
dc.contributor.author | 정인재 | ko |
dc.contributor.author | 이덕주 | ko |
dc.date.accessioned | 2015-11-20T12:35:32Z | - |
dc.date.available | 2015-11-20T12:35:32Z | - |
dc.date.created | 2014-01-15 | - |
dc.date.created | 2014-01-15 | - |
dc.date.issued | 2013-08 | - |
dc.identifier.citation | 한국군사과학기술학회지, v.16, no.4, pp.481 - 485 | - |
dc.identifier.issn | 1598-9127 | - |
dc.identifier.uri | http://hdl.handle.net/10203/201573 | - |
dc.description.abstract | Rotor 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.language | Korean | - |
dc.publisher | 한국군사과학기술학회 | - |
dc.title | 포텐셜 패널과 와류 조각 연계방법을 이용한 로터 공력 해석 | - |
dc.title.alternative | Potential Panel and Vortex Particle Coupling Analysis | - |
dc.type | Article | - |
dc.type.rims | ART | - |
dc.citation.volume | 16 | - |
dc.citation.issue | 4 | - |
dc.citation.beginningpage | 481 | - |
dc.citation.endingpage | 485 | - |
dc.citation.publicationname | 한국군사과학기술학회지 | - |
dc.identifier.kciid | ART001798797 | - |
dc.contributor.localauthor | 이덕주 | - |
dc.contributor.nonIdAuthor | 장지성 | - |
dc.contributor.nonIdAuthor | 정인재 | - |
dc.subject.keywordAuthor | Rotor(회전날개) | - |
dc.subject.keywordAuthor | Vortex method(와류방법) | - |
dc.subject.keywordAuthor | Aerodynamics(공기역학) | - |
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