Peter,
the idea of your table is good, but the values should be calculated where possible.
For example, the precession torque in level flight can be calculated as follows:
The moment of inertia J of a propeller (two or more blades) can be estimated by J=1/12 * mass * D^2.
If the mass of the prop is 24 grams, and D is 12 inch, then J prop=1/12*0,024 kg *0,1 m^2=0,0002 kg m^2.
The rotating part of an outrunner motor, dia 42 mm, will have a mass of about 0,1 kg. Assuming the rotor is 4 mm thick, we can use the formula for the inertia of a cylinder, J rotor= 1/2 m (r1^2 + r2^2). This leads to J rotor=1/2*0,1(0,021^2+0,017^2) = 0,0000 kg m^2.
Total J = J prop +J rotor =0,00024 kg m^2.
The precession torque T (horizontal level flight) is T= J * omega1 * omega 2, where the omegas are 2*pi*rev/second.
So, assuming 9000 rev/min and a lap time of 5,3 seconds, we obtain omega1=9000/60 *2*pi, and omega2=2*pi/5.3
If you then fill in the values for J, omega1 and omega 2 you obtain T=0,27 Newton*meter
For tractor props this torque is nose up, for pusher nose down.
Please let me know if you agree to this strategy. If you agree, I can continue to calculate the horizontal and vertical forces, and the resistance moments for tractor and pusher.
Regards,
Wolfgang