I am not saying I dont see the theory, We were just told not to teach it. I didnt write the rules, I was just a mushroom!!! kept in the dark and fed ! Thats what they wanted :dunno:
Just seems silly to not teach this very important part of aerodynamics to me. I am not saying you don't know or don't agree, nor am I attempting to argue with you. I am simply trying to give you the ammunition you need to discuss this with them. It isn't a theory, it is known to exist.
Consider this: An aircraft in a torque roll.
First, for some background information: torque is a rolling, not a yawing tendency. Hence the torque roll.
P-factor is not an issue since there is no AOA associated with a torque roll. The relative wind hits the prop perfectly straight on so both the up-going and down-going blades are at the same angle.
Gyro precession has never been a left yawing tendency. It can be a pitching or yawing tendency, in either direction, depending on the application of force.
All that is left is spiraling slipstream. The slower your aircraft is moving through the air the larger this effect is on the aircrafts tail. A torque roll has zero forward speed and hence the greatest effect from spiraling slipstream.
For proof, click this
torque roll video and go to about 42 seconds in. In the initial entry, a perfect torque roll. Notice the repeat taps of right rudder being used. The pilot does this to counter spiraling slipstream. At about 52/53 seconds he overdoes it and has to use some left rudder, but the initial is still visible.
I don't know if we have any aero pilots that actually perform this trolling these forums. If we do they can attest to the constant right rudder needed in this maneuver. I never had the pleasure of flying an aircraft capable of this, I learned about it through my RC flying.
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If you need more information, here:
Aerodynamics for Naval Aviators page 294:
"Slipstream Rotation. A critical directional control requirement may exist when the propeller powered airplane is at a high power and low airspeed. .... the single engine rotation propeller induces a slipstream swirl..."
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Flight Theory for Pilots page 250:
"Slipstream Rotation. This effect is predominant in single engined propeller aircraft. It may be critical at high power and low airspeed combinations, thus it is important during takeoff and landing operations. The slipstream from the propeller rotates about the fuselage..."
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Emergency Maneuver Training page 28:
"Spiral Slipstream. A spiral slipstream of air rotates clockwise behind the turning prop. ... Propeller slipstream can contribute significant left yaw, especially during slow flight at high power settings."
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Hope this can help you convince them of it's existence. I am digging through a more advanced aero book. But due to my lack of recent work with calculus I am having issues understanding the information to present it. However, for the time being this might get you started. Along with the NASA confirmation I don't see how your chief instructor can possibly tell you it doesn't exist and not to teach it.
I would appreciate any feedback from his concerns if you do discuss it with him/her.