Hi, I edited my statement but wanted to ask you if my thinking is correct here:
... it seems a significant benefit that the motor has peak torque at zero rpm and reaches peak power (still at peak torque) at 3600 rpm and maintains peak power throughout rpm increase. So, if we sized a prop for 4000 rpm with enough blade angle that we use max torque spinning at 3600 at standstill, and as forward motion eases the torque load on the prop and increasing rpm, we still are at max power, and maintain max power throughout takeoff just as if we had a constant speed prop. Am I talking out my trailing edge again or does this make sense?
Thanks
T