On a four propeller/engine wing, I’m wondering if theoretically at least, you could have a larger engine near the root of the wing with smaller engine(s) further out on the span..?.. If you could have the smaller propellers further out spin faster on smaller diameters and counter-rotate them... It's a pretty high wing so we can vary the prop diameter pretty well. The airframe design already has lots of vertical stabilization opportunities.
The engines would be diesel operating, generally at high torque at the 1500-2350 rpm range (further out on the wing engines would be rotating faster with high pitch at about 2200 rpm during cruise). On such a wing with different sized and powered engines would it be feasible to balance the torque-roll effects with computers (to calculate roll, yaw and pitch (relative to the NE Downframe?) angles on the fly), accelerometer sensors (arduino), spacing of the engines, construction of wings, vertical surfaces, tip tanks in the wings and air frame and rotating speed to rotating mass per diameter to feathered mass differentiation, etc.,?
Thanks so much, Greg