This work shows a UAV (Unmanned Aerial Vehicle) modeling of a fixed wing type and a delta wing configuration. The selection of an aerodynamic profile and the aircraft dimension was chosen. On a CAD package the geometric design was created, where the finite element analysis and fluid dynamics shows that the behavior of the aircraft follows the parameters required to be functional to manufacture and assemble their components.
Design of a Delta Wing Aircraft
2017-11-01
517271 byte
Conference paper
Electronic Resource
English