БЕЗПІЛОТНИЙ ЛІТАЛЬНИЙ АПАРАТ ІЗ ПРЯМИМ ТА АРОЧНИМ КРИЛОМ
Journal Title: Механіка гіроскопічних систем - Year 2015, Vol 0, Issue 30
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.
Authors and Affiliations
Андрій Ігорович , Зоренко, Геннадій Анатолійович Вірченко
Keywords
Related Articles
- EP ID EP540118
- DOI -
- Views 76
- Downloads 0
Adaptive winglet
Winglet are intended to improve the efficiency of fixed-wing aircraft by reducing inductive drag. Such devices increase the effective aspect ratio of a wing without materially increasing the wingspan. Winglets provide fu...
Approximate methods for assessing the recovery factor in the collision of elastic bodies
We consider the elementary theory, which explains the presence of Newton recovery factor at the collision of elastic bodies, which, as shown by the authors, is less than unity. The existence of a recovery factor less tha...
Автомобильные защитные наноматериалы
<p>Приведены результаты анализа современных разработок, проблем и перспектив применения защитных наноматериалов на автомобильном транспорте. В работе дан обзор инновационных автомобильных лакокрасочных наноматериалов, по...
BENDING OF COMPOSITE SHELLS BASED ON NON-LINEAR DISTRIBUTION OF DISPLACEMENTS ACROSS THE THICKNESS OF FILLER
This paper presents a methodology of calculation the composite laminated shells, which is based on the variational-grid approach of forming the necessary functionals. Further minimizing of them was performed by the coord...
Теоретические и экспериментальные исследования ошибок трехосного и одноосного гирокомпасов на основе лазерных гироскопов
<p>Рассматриваются некоторые задачи, возникающие при создании бесплатформенной инерциальной навигационной системы (БИНС) в режиме начальной выставки на неподвижном основании. На примере вычисления азимута с помощью одно...