Sorry to flog this one but it was niggling me & thought it might be of interest to us weekend physicists.
I dug out some old notes.
There are 4 forces tending to yaw a plane on t/o.
1. Reactive force. See my contribution above.
2. Slipstream effect. Beautifully described by Wilbus.
3. Gyroscopic precession. Spinning mass of propellor & engine makes them subject to this effect. If a force is applied to a spinning gyroscope, the gyroscope acts as if the force were applied at a point 90 deg to the direction of rotation. When nose goes down on take-off gyroscopic precession pushes nose to left. Those old enough to remember toy gyroscopes spinning on bits of string will know what I mean
4. P-factor (asymmetric blade effect). In a tail dragger the downward moving prop blade has a higher angle of attack & thus produces more thrust. When props rotating clockwise (as viewed from cockpit) this yaws plane to left.
Corsair scores badly on all these because
1. Big rotary engine (1 & 3)
2. Big diameter prop (2)
3. Tail dragger (4)
P38 suffers little from yaw on take off 'cos inline contra-rotating engines & horizontal AoA (tricycle u/c) on take-off.
Regards