The invention provides an aerodynamic layout of a drone aircraft and belongs to the field of aerodynamic layout design technology of air vehicles. The aerodynamic layout is provided with a front edge strip used for high-attack angle flying and two steering-free air inlets, an aircraft body for optimizing the aerodynamic characteristics, a low-aspect ratio wing with a thin win and a cambered face, horizontal tail ands and a vertical tail. Thus, maneuvering characteristics and high angle of attack flying ability of the drone aircraft are greatly improved.
Aerodynamic layout of drone aircraft
2015-09-09
Patent
Elektronische Ressource
Englisch
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