The “static temperature at the exit where the flow is supersonic,” denoted as Te, refers to the temperature of the fluid at the exit of a nozzle or flow passage when the flow velocity exceeds the speed of sound and enters supersonic conditions. Static temperature refers to the temperature of the fluid at rest (not moving).Â
- Ratio of static temperature at exit to the inlet temperature (Te/T0)
- Inlet temperature (T0) in N/m^2
- Static temperature at exit (Te) in N/m^2