02.2 - Experimental Aerodynamics
EFFECTS OF PROPELLER LOCATIONS ON THE VORTEX SYSTEM ABOVE DELTA-SHAPED UAV MODEL
K.A. Kasim¹, S. Mat¹, I.S. Ishak¹, M. Said¹; ¹Universiti Teknologi Malaysia, Malaysia
A 55°sharp-edged non-slender delta wing UAV model is studied experimentally at low speed wind tunnel conditions. The model will be tested by including three propeller configurations pusher, tractor and middle. The study will be focused on effects of propeller locations on aerodynamic characteristics and vortex system of the UAV.