Pull-Up Maneuver Rate evaluator uses Turn Rate = [g]*(Pull-Up Load Factor-1)/Pull-Up Maneuver Velocity to evaluate the Turn Rate, The Pull-up Maneuver Rate quantifies the rate at which an aircraft ascends during a pull-up maneuver. This formula calculates the turn rate based on gravitational acceleration, the load factor during the pull-up maneuver, and the velocity during the pull-up. Understanding and applying this formula is crucial for pilots and engineers to optimize the ascent rate. Turn Rate is denoted by ω symbol.
How to evaluate Pull-Up Maneuver Rate using this online evaluator? To use this online evaluator for Pull-Up Maneuver Rate, enter Pull-Up Load Factor (npull-up) & Pull-Up Maneuver Velocity (Vpull-up) and hit the calculate button.