Total Drag for given Excess Power evaluator uses Drag Force = Thrust-(Excess Power/Velocity) to evaluate the Drag Force, The Total Drag for given Excess Power represents the total drag force experienced by the aircraft during climb flight, which is the difference between the thrust produced by the engines and the excess power used to generate additional thrust for the climb. Drag Force is denoted by FD symbol.
How to evaluate Total Drag for given Excess Power using this online evaluator? To use this online evaluator for Total Drag for given Excess Power, enter Thrust (T), Excess Power (Pexcess) & Velocity (v) and hit the calculate button.