Results 1 to 10 of about 30 (30)
Авіаційно-космічна техніка та технологія, 2022 This article presents the structure of designing and modeling the flow of rotors and pusher propellers in a highly rarefied atmosphere. The aerodynamic characteristics of an airfoil are key factors in determining design accuracy and performance ...
Mykola Kulyk +4 more
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EFFECT OF THE CLEARANCE BETWEEN ROWS OF COAXIAL PROPFAN ON THRUST
Авіаційно-космічна техніка та технологія, 2020 The thrust of a turboprop engine depends on many factors, one of which is hydraulic loss when flowing around the propeller blades. When using coaxial propellers, this factor plays an even greater role, since in this case the losses associated with the ...
Вячеслав Юрьевич Усенко +2 more
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Efficiency of tandem UAV propulsion fans with toroidal-helical connected blade tips
Авіаційно-космічна техніка та технологіяUnmanned Aerial Vehicles (UAVs) are increasingly in demand for both civilian and military missions. This has become especially evident during combat operations against the Russian Federation’s occupying forces, where battlefield advantages have been ...
Mykola Kulyk +3 more
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Assessment of the thrust force of UAV slotted propellers
Авіаційно-космічна техніка та технологіяThe thrust characteristics of slotted propellers of an unmanned aerial vehicle are the subject of the study. The study object is a slotted propeller of an unmanned aerial vehicle.
Liubov Markovska +2 more
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Системи озброєння і військова технікаПредставлено експериментальну методику визначення аеродинамічних характеристик повітряного гвинта НГ-1 на гвинтовому приладі ГП-1, склад та технічні характеристики експериментального обладнання.
В.А. Безпалий +1 more
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Compact stand for testing single propellers of mini- and micro- unmanned aerial vehicles
Авіаційно-космічна техніка та технологіяThis paper presents the development of a stand for the experimental testing of single propellers designed for mini- and micro-unmanned aerial vehicles (UAVs).
Maksym Borysiuk, Yakiv Rudkin
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Topological optimization of a ducted propeller of UAV
Авіаційно-космічна техніка та технологіяThe subject of this study is the minimization of the duct mass for a ducted propeller of UAV. The object of this study is a two-bladed ducted quadcopter propeller. The peripheral diameter of the propeller is 128 mm, and the hood is 2 mm thick.
Anton Balalaiev +4 more
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Normal characteristics of a UAV air slot propeller
Авіаційно-космічна техніка та технологіяThis paper presents the results of a numerical study of the influence of passive control of the boundary layer around the propeller blade by creating cuts (slits) in the body of the propeller blade of the type 1045, which is widely used in unmanned ...
Lyubov Markovska
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