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dc.contributor.authorHedayatpour, Mojtaba
dc.contributor.authorMehrandezh, Mehran
dc.contributor.authorJanabi-Sharifi, Farrokh
dc.date.accessioned2018-11-06T14:37:53Z
dc.date.available2018-11-06T14:37:53Z
dc.date.issued2018-05
dc.identifierCSME216
dc.identifier.issn978-1-77355-023-7
dc.identifier.urihttp://hdl.handle.net/10315/35255
dc.identifier.urihttp://dx.doi.org/10.25071/10315/35255
dc.description.abstractThis paper presents mathematical modeling for thrust force and moments generated by a propeller. In particular, the effects of freestream on propeller’s performance are investigated. We introduce some of the applications of the proposed model in modeling multi-rotor UAVs which helps to increase stability or maneuverability of the vehicle. In the end, simulation results for thrust force and moments of an example propeller in presence of a uniform freestream are presented.
dc.language.isoenen_US
dc.publisherCSME-SCGMen_US
dc.rightsThe copyright for the paper content remains with the author.
dc.subjectMechatronicsen_US
dc.subjectRobots and Controlen_US
dc.subjectComponent
dc.subjectPropeller
dc.subjectAerodynamics
dc.subjectThrust force
dc.subjectUnmanned aerial vehicles
dc.subjectFreestream
dc.titlePropeller Performance In Presence Of Freestreamen_US
dc.typeArticleen_US


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