Aircraft Engineering
Аuthors
1*, 2**, , ***1. Institution of Russian Academy of Sciences Dorodnicyn Computing Centre of RAS, 40, Vavilov st., Moscow, 119333, Russia
2. Kompani «INREA», 39-1, Kronshtadtsky blv., Moscow, 125499, Russia
*e-mail: i.voronich@yandex.ru
**e-mail: sakolchev@gmail.com
***e-mail: vtkachenko@skc.ru
Abstract
Purpose of present work is to form requirements for small-sized unmanned aircraft suitable for extensive radiation and ecological area monitoring in the field. Paper includes short review of designs, aerodynamic and technical characteristics of small- and middle-sized aircrafts for generalization of research results. Aspects of realization of such aircrafts in aerodynamical shapes, propulsion unit, and service load are considered. Prototype and ways of its modification to meet formulated requirements are defined. Fundamentals of computational technique for computational-experimental research are discussed. Example of technique application is givenKeywords:
unmanned aircraft, monitoring, aerodynamics
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