Konu "Uav Propulsive Systems" için Rektörlüğe Bağlı Birimler listeleme
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Performance of a ducted propeller designed for UAV applications at zero angle of attack flight: An experimental study
(Elsevier France-Editions Scientifiques Medicales Elsevier, 2015)Performance characteristics and velocity field of a 16 inch diameter ducted propeller are investigated experiinentally using five different duct shapes. Experiments are conducted at zero angle of attack which simulates ...