Velocity for given Pull-Up Maneuver Radius evaluator uses Pull-Up Maneuver Velocity = sqrt(Turn Radius*[g]*(Load Factor-1)) to evaluate the Pull-Up Maneuver Velocity, The Velocity for given Pull-Up Maneuver Radius of an aircraft is dependent upon the maneuver radius and load factor of the aircraft, this formula provides a simplified approximation of the velocity needed to maintain the desired descent rate during the pull-up maneuver. Pull-Up Maneuver Velocity is denoted by Vpull-up symbol.
How to evaluate Velocity for given Pull-Up Maneuver Radius using this online evaluator? To use this online evaluator for Velocity for given Pull-Up Maneuver Radius, enter Turn Radius (R) & Load Factor (n) and hit the calculate button.