In aircraft design and engineering, “V_inlet” represents the velocity of the fluid (typically air) at the inlet of a component or system, such as a compressor, inlet duct, or air intake.
The formula for calculating V_inlet can be defined as:
- V_inlet is the velocity of the fluid at the inlet, 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.
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