DocumentCode
3704966
Title
Aerodynamic and flight characteristics of prospective UAV scheme “flying wing”
Author
O.L. Lemko;O.D. Molodchyk
Author_Institution
National Technical University of Ukraine ?Kyiv Polytechnic Institute?, Ukraine
fYear
2015
Firstpage
33
Lastpage
36
Abstract
This paper is devoted to the results of studies prospective unmanned aerial vehicle scheme “flying wing”. Using aerodynamic configuration “flying wing”, which force greater than that of aircraft of the normal circuit losses balancing aerodynamic qualities are still not widely available in aviation, but “flying wing” allows you to fully realize their positive properties to create a new generation of unmanned aerial vehicles.
Keywords
"Aerodynamics","Unmanned aerial vehicles","Aircraft","Engines","Force","Payloads","Drag"
Publisher
ieee
Conference_Titel
Actual Problems of Unmanned Aerial Vehicles Developments (APUAVD), 2015 IEEE International Conference
Print_ISBN
978-1-4673-6566-6
Type
conf
DOI
10.1109/APUAVD.2015.7346552
Filename
7346552
Link To Document