Velocity of Aircraft for given Excess Power evaluator uses Velocity = Excess Power/(Thrust-Drag Force) to evaluate the Velocity, The Velocity of Aircraft for given Excess Power is the airspeed required to maintain a given rate of climb, considering the excess power available and the balance between thrust and drag forces during climb flight. Understanding and applying this formula is crucial for pilots and engineers to optimize climb performance. Velocity is denoted by v symbol.
How to evaluate Velocity of Aircraft for given Excess Power using this online evaluator? To use this online evaluator for Velocity of Aircraft for given Excess Power, enter Excess Power (Pexcess), Thrust (T) & Drag Force (FD) and hit the calculate button.