%0 Journal Article
%T Design and Optimization of Wing Structure for a Fixed-Wing Unmanned Aerial Vehicle (UAV)
%A Jiawen Yu
%J Modern Mechanical Engineering
%P 249-263
%@ 2164-0181
%D 2018
%I Scientific Research Publishing
%R 10.4236/mme.2018.84017
%X The wing, one of
the most important parts of aircraft, always requires sophis-ticated design to
increase lift, reduce drag and weight. For modern fixed-wing UAV, extending
cruising time is always a requirement for the overall design. Designing a most
light wing that can match the requirements of work condi-tions is desired. In
this work, according to the work conditions, we compare several types of wing
and chose beam-type wing. Then we made the detailed design and optimization to
reduce the weight of wing. At last, we draw the 3D model for potential
realistic production.
%K Wing Structure
%K Optimization
%K 3D Model Design
%U http://www.scirp.org/journal/PaperInformation.aspx?PaperID=88625