БЕЗПІЛОТНИЙ ЛІТАЛЬНИЙ АПАРАТ ІЗ ПРЯМИМ ТА АРОЧНИМ КРИЛОМ

Abstract

The purpose of this article is to develop a methodology for calculating the aerodynamic computer of the aircraft to straight and arched wings.Сorresponding unmanned aerial vehicle has been considered for the development of methodology. This design is necessary to achieve greater lift force which enables the implementation of a vertical takeoff and landing.Scientific novelty lies in the combination of design already exist-ing of aircraft with arched wings and multicopter, implement-ing vertical takeoff.This article describes a method of computer calculation of aerodynamic-cal characteristics for unmanned aircraft to straight and arched wings. To develop a methodology for the selection of the profile were used, calculation of aerodynamic characteristics for an isolated wing, as well as the construction of the velocity diagrams and overloads for further Designing-of unmanned aircraft to straight and arched wings.According to the calculation results it can be concluded that the subject of the summer-tive device can perform a vertical take-off and landing on nepod-prepara- areas and in urban environments.