In aircraft design and engineering, “V_outlet” represents the velocity of the fluid (typically air) at the outlet of a component or system, such as a compressor, nozzle, or exhaust.
The formula for calculating V_outlet can be defined as:
- V_outlet is the velocity of the fluid at the outlet, typically measured in meters per second (m/s) or other velocity units.
- P_total_outlet is the total pressure at the outlet, typically measured in pascals (Pa) or other pressure units.
- P_static_outlet is the static pressure at the outlet, typically measured in pascals (Pa) or other pressure units.
- ρ (rho) is the density of the fluid at the outlet, typically measured in kilograms per cubic meter (kg/m³) or other density units.