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Performance of a ducted propeller designed for UAV applications at zero angle of attack flight: An experimental study

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dc.contributor.authorKavsaoğlu, Mehmet Şerif
dc.contributor.authorD. Erdem
dc.contributor.authorMehmet Şerif Kavsaoğlu
dc.contributor.orcid0000-0002-4789-6663
dc.contributor.orcid0000-0002-0735-0869
dc.date.accessioned2025-11-13T09:25:45Z
dc.date.issued2015-06-13
dc.identifier.doihttps://doi.org/10.1016/j.ast.2015.06.005
dc.identifier.endpage386
dc.identifier.issn1270-9638
dc.identifier.openalexW577964763
dc.identifier.startpage376
dc.identifier.urihttps://hdl.handle.net/11421/1113
dc.identifier.urihttps://doi.org/10.1016/j.ast.2015.06.005
dc.identifier.volume45
dc.language.isoen
dc.relation.ispartofAerospace Science and Technology
dc.rightsrestrictedAccess
dc.subjectDuct (anatomy)
dc.subjectThrust
dc.subjectTakeoff
dc.subjectAdvance ratio
dc.subjectTakeoff and landing
dc.subjectMechanics
dc.subjectPropeller
dc.subjectFreestream
dc.subjectTorque
dc.subjectAerospace engineering
dc.subjectStatic pressure
dc.subjectAcoustics
dc.subjectBlade pitch
dc.subjectTurbulence
dc.subjectMarine engineering
dc.subjectEngineering
dc.subjectPhysics
dc.subjectReynolds number
dc.subjectTurbine
dc.subject.sdg7
dc.titlePerformance of a ducted propeller designed for UAV applications at zero angle of attack flight: An experimental study
dc.typeArticle
dspace.entity.typePublication
local.authorid.openalexA5042277913

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