Investigation of the Influence of Geometrical Parameters on The Take-off Mass of Unmanned Aircraft Wing

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dc.contributor.authorJinadu Abdulbaqi
dc.contributor.authorTiniakov Dmytro
dc.contributor.authorKoloskov Volodymyr
dc.date.accessioned2023-07-14T14:28:35Z
dc.date.available2023-07-14T14:28:35Z
dc.date.issued2014-10-24
dc.description.abstractThe aim for carrying out investigation on the wing parameters of an unmanned aircraft take-off mass is to look for its geometrical and structural weakness so as to be able calculate and deduce new parameters that will increase the general performance of the aircraft, thus reducing its take-off mass. These parameters include the relative airfoil thickness, aspect ratio, taper ratio and sweep angle. Along the line in the research, limits are used to define load factor and landing speed. These limits are used, as when displayed on the graph, give the ability to determine the minimal mass within the limit range.
dc.identifier.urihttps://kwasuspace.kwasu.edu.ng/handle/123456789/290
dc.language.isoen
dc.publisherАКТУАЛЬНІ ПИТАННЯ СУЧАСНОЇ НАУКИ. ІІ МІЖНАРОДНА НАУКОВО-ПРАКТИЧНА КОНФЕРЕНЦІЯ
dc.titleInvestigation of the Influence of Geometrical Parameters on The Take-off Mass of Unmanned Aircraft Wing
dc.typeTechnical Report
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