Stearman...no fighters, not yet.
But P-factor is present in all prop airplanes, with the notable exception of twins with counter-rotating propellers. So, as an example, the Grumman E-2 (which I was qualified to fly) has quite a bit of P-factor. Both T56 turboprop engines rotate the same direction, making the left engine the critical one (Because, if it fails, the P-factor adds to the yaw from the thrust of the right engine, so more airspeed at full rudder is required to control the plane, and that defines VMCA...a right engine failure is easier because the P-factor counters some of the yaw).
There is an immediate torque roll when the engine accelerates, but that's not the same as P-factor.
It's not just torque that you're countering with that initial trim.
But P-factor is present in all prop airplanes, with the notable exception of twins with counter-rotating propellers. So, as an example, the Grumman E-2 (which I was qualified to fly) has quite a bit of P-factor. Both T56 turboprop engines rotate the same direction, making the left engine the critical one (Because, if it fails, the P-factor adds to the yaw from the thrust of the right engine, so more airspeed at full rudder is required to control the plane, and that defines VMCA...a right engine failure is easier because the P-factor counters some of the yaw).
There is an immediate torque roll when the engine accelerates, but that's not the same as P-factor.
It's not just torque that you're countering with that initial trim.