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dc.contributor.authorYılmaz, S.
dc.contributor.authorErdem, D.
dc.contributor.authorKavsaoğlu, Mehmet Şerif
dc.date.accessioned2019-10-18T19:02:48Z
dc.date.available2019-10-18T19:02:48Z
dc.date.issued2013
dc.identifier.isbn9781624101816
dc.identifier.urihttps://hdl.handle.net/11421/10850
dc.descriptionAmerican Institute for Aeronautics and Astronautics (AIAA)en_US
dc.description51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition 2013 -- 7 January 2013 through 10 January 2013 -- Grapevine, TX -- 98224en_US
dc.description.abstractPerformance characteristics and velocity field of a ducted propeller in hover and axial flight conditions are investigated experimentally. Five different circular duct shapes has been tested. Effect of duct geometry is studied by means of measurements at various flow conditions. Velocity field upstream and downstream of the propeller, axial force acting on each component of the propulsive system, rotor speed and torque are measured. Pressure distribution on duct inner and outer surfaces is also investigated. Experimental results obtained for open and ducted propellers are compareden_US
dc.language.isoengen_US
dc.rightsinfo:eu-repo/semantics/closedAccessen_US
dc.titleEffects of duct shape on a ducted propeller performanceen_US
dc.typeconferenceObjecten_US
dc.relation.journal51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition 2013en_US
dc.contributor.departmentAnadolu Üniversitesien_US
dc.relation.publicationcategoryKonferans Öğesi - Uluslararası - Kurum Öğretim Elemanıen_US


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