Angular Velocity of a Pull-down Maneuver Calculator

The angular velocity of a pull-down maneuver is the rate at which the aircraft rotates during a downward pitch maneuver. It measures the change in the aircraft’s orientation over time, typically expressed in radians per second. This angular velocity is influenced by factors such as the aircraft’s airspeed, load factor.

Where:

$\omega$ is the angular velocity (in radians per second),

$g$ is the acceleration due to gravity (approximately 9.81 m/s^),

$n$ is the load factor,

$V$ is the true airspeed of the aircraft (in meters per second or feet per second).