DocumentCode
670265
Title
Experimental investigation of aerodynamic performance of a small UAV with a telescopic wing
Author
Kryvokhatko, I.S. ; Sukhov, V.V.
Author_Institution
Nat. Technic Univ. of Ukraine KPI, Kiev, Ukraine
fYear
2013
fDate
15-17 Oct. 2013
Firstpage
17
Lastpage
20
Abstract
Telescopic wing is the mechanism aimed to increase lift-to-drag ratio of aircraft or UAV by increasing wing aspect ratio. In previous study theoretical mathematical models of the aerodynamic performance of the telescopic wing UAV for low Reynolds number were developed. The present study investigates these characteristics experimentally.
Keywords
aerodynamics; aerospace components; autonomous aerial vehicles; robot dynamics; vehicle dynamics; Reynolds number; aerodynamic performance; aircraft lift-to-drag ratio; small UAV; telescopic wing; unmanned aerial vehicle; Aerodynamics; Atmospheric modeling; Conferences; Drag; Mathematical model; Unmanned aerial vehicles; Visualization; induced drag; lift-to-drag ratio; low Reynolds number; telescopic wing;
fLanguage
English
Publisher
ieee
Conference_Titel
Actual Problems of Unmanned Air Vehicles Developments Proceedings (APUAVD), 2013 IEEE 2nd International Conference
Conference_Location
Kiev
Print_ISBN
978-1-4799-3305-1
Type
conf
DOI
10.1109/APUAVD.2013.6705272
Filename
6705272
Link To Document