Aerodynamic Evaluation of UiTM’s Blended Wing Body Unmanned Aerial Vehicle at Different Elevon Configurations using Vortex Lattice Method
This paper presents findings of the preliminary aerodynamic evaluation for UiTM’s baseline model blended wing body (BWB) unmanned aerial vehicle (UAV). The UAV design is based on a new planform and hence its characteristics were yet to be understood. The design is tailless, with both the inboard and...