倾转机翼无人机气动设计与分析

Aerodynamic Design and Analysis of Tilting Wing UAV

垂直起降固定翼无人机是当下无人机发展的趋势之一。倾转机翼无人机作为其重要的一个分支,在国内外均有一定程度的发展。论文参考NASA倾转机翼无人机GL-10的构型,建立了理论计算结合XFLR5气动估算软件分析的设计方法,并对倾转机翼无人机进行设计和分析,证明了该设计方法的可行性。

Vertical take-off and landing fixed-wing UAV is one of the current development trends of unmanned aerial vehicles(UAVs).As an important branch of UAVs,tilt wing UAVs have been developed to a certain extent at home and abroad.In this paper,referring to the configuration of NASA tilt wing UAV GL-10,a design method combining theoretical calculation and XFLR5 aerodynamic estimation software analysis was established,and the design and analysis of the tilt wing UAV proved the feasibility of the design method.