Prediction of Wake Structure and Induced Velocity of a Helicopter Rotor in the Vortex Ring State using a Vortex Particle Method

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dc.contributor.authorPark, Sehwanko
dc.contributor.authorLee, Duck-Jooko
dc.date.accessioned2015-01-29T05:08:10Z-
dc.date.available2015-01-29T05:08:10Z-
dc.date.created2014-12-22-
dc.date.issued2014-12-18-
dc.identifier.citation3rd Asian-Australian Rotorcraft Forum (ARF)-
dc.identifier.urihttp://hdl.handle.net/10203/193287-
dc.languageEnglish-
dc.publisherAsian-Australian Rotorcraft Forum-
dc.titlePrediction of Wake Structure and Induced Velocity of a Helicopter Rotor in the Vortex Ring State using a Vortex Particle Method-
dc.typeConference-
dc.type.rimsCONF-
dc.citation.publicationname3rd Asian-Australian Rotorcraft Forum (ARF)-
dc.identifier.conferencecountryAT-
dc.identifier.conferencelocationMelbourne Convention and Exhibition Centre-
dc.contributor.localauthorLee, Duck-Joo-
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AE-Conference Papers(학술회의논문)
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