What is 'P-factor' (asymmetric blade effect) and when is it most pronounced in a single-engine propeller aircraft?
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A
Gyroscopic precession when yawing; most pronounced at high speed in level flight
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B
The descending blade produces more thrust than the ascending blade; most pronounced at high power and high angle of attack
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C
Propeller torque reaction; most pronounced during cruise at altitude
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D
Slipstream effect on the vertical stabilizer; most pronounced during sideslip