In aircraft design and engineering, “T_inlet” represents the absolute temperature of the air at the inlet of a component or system, such as a compressor or an engine. Absolute temperature is typically measured in kelvin (K) or other temperature units.
The formula for calculating the absolute temperature at the inlet (T_inlet) is based on the Celsius (°C) temperature converted to kelvin:
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- T_inlet (in kelvin) is the absolute temperature at the inlet, measured in kelvin (K).
- T_inlet (in degrees Celsius) is the temperature at the inlet measured in degrees Celsius (°C).