What is the term for the phenomenon that combines the effects of P-factor, accelerated slipstream, and torque in multi-engine aircraft operations?

The correct term that encompasses the combined effects of P-factor, accelerated slipstream, and torque in multi-engine aircraft operations is widely recognized as asymmetrical thrust. This phenomenon occurs when the thrust produced by the engines is not equal on both sides of the aircraft, primarily due to the influence of each of these factors.

P-factor is caused by the greater angle of attack on the descending blade of a propeller compared to the ascending blade, resulting in uneven thrust when an aircraft yawing occurs. Accelerated slipstream refers to the increased velocity of airflow caused by the propellers, particularly in multi-engine configurations, which can also lead to asymmetrical forces acting on the aircraft. Torque, a result of the rotational motion of the propellers, leads to a turning tendency that can create uneven lifting forces depending on the aircraft's configuration and power settings.

The term P.A.S.T. is not a standard terminology associated with these aerodynamic effects, making it less appropriate. Engine Feedback Loop might suggest that the engines are influencing each other through their thrust changes, but does not accurately describe the individual phenomena leading to asymmetrical thrust. Slipstream Dynamics, while related to the airflow patterns around the aircraft influenced by the propellers, does not specifically capture the notion of the resulting thrust