The Dynamic Pressure at the Compressor Exit in aircraft design refers to the pressure caused by the motion of the air leaving the compressor section of a gas turbine engine. It is a crucial parameter for assessing the kinetic energy of the airflow at this point in the engine.
The formula for calculating Dynamic Pressure (q) at the Compressor Exit is the same as the one used for the compressor inlet:
- ρ (rho) represents the air density at the compressor exit and is typically measured in kilograms per cubic meter (kg/m³).
- V represents the velocity of the air leaving the compressor at the exit, typically measured in meters per second (m/s).