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Trade Study 2. Motor Selection and propeller matching. Hadrien guepet. Propulsion System. brushless electric motor modelling. Power Diagram. ElectricPower (Bat). Mechanical power. Controller Loss. Iron loss due to hysteresis and eddy current. friction. Copper loss due to wiring.
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Trade Study 2 MotorSelection and propellermatching Hadrien guepet
brushlesselectricmotormodelling • Power Diagram ElectricPower (Bat) Mechanical power Controller Loss Iron loss due to hysteresis and eddy current friction Copper loss due to wiring
Comparaison between our model and experimental results After comparing 10 motors : 4% error max
Our Propeller : 12 x 8 APCE • Performance Chart :
Power required and propefficiency for our aircraft Design point : 25° at 40ft/s Power required for the propeller : 342W @ 8210 rpm
Motormatching • According to our model a motorwith a KV of 977 will match perferctlyexactly • The closest possible choiceis a 1000KV motor • Wechoose The Turnigy SK 3548 1050KV • (the smaller SK 3542 could fit but wewant to be sure it
Selectedmotor • TurnigyAerodrive SK 3548 --- 1050 KV
Efficiencydiagrams https://www.youtube.com/watch?v=GrrJoOSR4W8
Aircraft performance Max speed about 83 ft/s Max climb speed = 40 ft/s
Speed diagram 83 ft/s 40 ft/s 45 ft/s 22,5 ft/s 49 ft/s 20 ft/s Stall Speed Choosencruise speed Speed for max Vz (19ft/s max) Speed for max angle of climb (33°) Max speed in level flight Max speed at 25° of climb