Design of the propeller for tilt-rotor UAV

dc.contributor.authorKlesa, Jan
dc.contributor.editorLukeš, Vladimír
dc.contributor.editorRendl, Jan
dc.contributor.editorHajžman, Michal
dc.contributor.editorByrtus, Miroslav
dc.date.accessioned2018-04-17T06:24:37Z
dc.date.available2018-04-17T06:24:37Z
dc.date.issued2018
dc.description.abstract-translatedTilt-wing and tilt-rotor unmanned aerial vehicles (UAVs) represents promising direction for the future development. This paper presents the method for the preliminary design optimization of the propeller for such vehicle. It should be capable to generate high thrust in both forward flight and hover modes. This brings design challenges for the propeller aerodynamic design. All considered variants have same number of blades, engine power, airfoils and diameter. Thrust in forward cruise speed 30 m/s and in hover is computed and compared by the means of Pareto diagram. Choose of the optimal RPM is based on the computation results.en
dc.format4 s.cs
dc.format.mimetypeapplication/pdf
dc.identifier.citation20th International Conference Applied Mechanics 2018: April 9-11, 2018, Myslovice, Czech republic: conference proceedings, p. 45-48.en
dc.identifier.isbn978-80-261-0766-8
dc.identifier.urihttp://hdl.handle.net/11025/29634
dc.language.isoenen
dc.publisherZápadočeská univerzita v Plznics
dc.rights© Západočeská univerzita v Plznics
dc.rights.accessopenAccessen
dc.subjectkonstrukce vrtulecs
dc.subjectVTOLcs
dc.subjectsklopné křídlocs
dc.subjectUAVcs
dc.subject.translatedpropeller designen
dc.subject.translatedVTOLen
dc.subject.translatedtilt-wingen
dc.subject.translatedUAVen
dc.titleDesign of the propeller for tilt-rotor UAVen
dc.typekonferenční příspěvekcs
dc.typeconferenceObjecten
dc.type.statusPeer-revieweden
dc.type.versionpublishedVersionen

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