Load Factor Given By Pull-Up Maneuver Radius Calculator

In flight mechanics, the load factor during a pull-up maneuver refers to the factor by which the total aerodynamic force on an aircraft exceeds its weight. This increase in load factor is a consequence of the aircraft’s acceleration upwards, resulting in greater gravitational forces acting on it. The formula to calculate Load Factor as follows:

Where:

  • V is the velocity in m/s,
  • R is the Turn Radius in m
  • g is the gravity in m/s2

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