04.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity
STRUCTURAL DESIGN AND ANALYSIS OF A QUADROTOR FIXED-WING HYBRID UAV WING
W. Fang, China; H. Ma, China; H. Zhang, China
This paper designs and analyses a hybrid layout UAV wing structure considering load condition of maneuvering and crosswind resisting situation. Analysis based on finite element model shows the structural performance of wing during flight and using stronger main spar can effectively increase wing twisting rigidity.