In the context of aircraft design, “Pout” typically refers to the output power of an aircraft engine or propulsion system. The output power represents the useful mechanical power generated by the engine or propulsion system, which may be used to drive the aircraft’s propellers or provide thrust.
The formula for output power (Pout) depends on the specific type of engine or propulsion system being used. For example:
For a Jet engine:Â
- Pout is the output power in watts (W).
- F is the thrust produced by the engine in newtons (N).
- V is the velocity of the aircraft in meters per second (m/s).
- η (eta) is the efficiency of the engine, typically expressed as a decimal or percentage.