In aircraft design and engineering, “T_outlet” 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_outlet) is based on the Celsius (°C) temperature converted to kelvin:
- T_outlet (in Celsius) is the absolute temperature at the inlet, measured in kelvin (K).
- T_outlet (in degrees Celsius) is the temperature at the inlet measured in degrees Fahrenheit (°F).