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P‑factor, also known as asymmetric blade effect and asymmetric disc effect, is an aerodynamic phenomenon experienced by a moving propeller, wherein the propeller's center of thrust moves off-center when the aircraft is at a high angle of attack. This shift in the location of the center of thrust will exert a yawing moment on the aircraft, causing it to…
Measurement, Effects & Helicopters
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propeller aircraft blade angle thrust attack disc engine speed flight forward yaw blades down-going rudder center greater power critical effect
| Subject | Predicate | Object | Confidence | Src |
|---|---|---|---|---|
| P-factor | related to Helicopters | The | 0.60 | section |
| P-factor | related to Helicopters | Helicopters | 0.60 | section |
| P-factor | related to Helicopters | If | 0.60 | section |
| P-factor | related to Helicopters | Gyroscopic | 0.60 | section |
| P-factor | related to Helicopters | VNE | 0.60 | section |
| P-factor | related to Multi engine propeller aircraft | For | 0.60 | section |
| P-factor | related to Multi engine propeller aircraft | P-factors | 0.60 | section |
| P-factor | related to Multi engine propeller aircraft | However | 0.60 | section |
| P-factor | related to Multi engine propeller aircraft | As | 0.60 | section |
| P-factor | related to Multi engine propeller aircraft | The | 0.60 | section |
| P-factor | related to Multi engine propeller aircraft | Thus | 0.60 | section |
| P-factor | related to Multi engine propeller aircraft | With | 0.60 | section |
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