In aircraft design and engineering, “P_total_outlet” represents the total pressure at the outlet of a component or system, such as a compressor or a nozzle. Total pressure is a combination of both static pressure and dynamic pressure, and it is a crucial parameter used to assess the performance and behavior of various aircraft components.
The formula for calculating P_total_outlet can be defined as:
- P_Total_Outet is the total pressure at the inlet, typically measured in pascals (Pa) or other pressure units.
- P_static_inlet is the static pressure at the inlet, typically measured in pascals (Pa) or other pressure units.
- ρ (rho) is the density of the fluid at the inlet, typically measured in kilograms per cubic meter (kg/m³) or other density units.
- V_inlet is the velocity of the fluid at the inlet, typically measured in meters per second (m/s) or other velocity units