Take-off characteristics for NACA 4612 aerofoil in a twin-wing configuration with optimum angles of attack
Unmanned Aerial Vehicles are used generally at low levels and speeds.The research reported in this article Machine Control investigates the possible use of twin-wing designs for higher altitudes with a focus on the possible lift capable for either short runways or high payloads.The wing aerofoil and unique Angles of Attack, AoA, are set 5o on the u