The Aerodynamic Design and Analysis of Small Tube-Launched Unmanned Aerial Vehicle
YANG Leisong;LI Songchao;The 27th Research Institute of China Electronics Technology Group Corporation;
Small tube-launched UAV is a new unmanned aerial vehicle,which has its special uses in battlefield. According to the characteristic of small tube-launched UAV,and tandem-wing aerodynamic configuration is constructed. And the numerical simulation method is applied to analyze the UAV lift-drag characteristics,longitudinal static stability and lateral and directional static stability. The conclusions indicated that the design fulfills objectives,which can be reference in design and study of the small tubelaunched UAV.
【CateGory Index】： V279