1.9.2. Inlet (Supersonic)

 

1.9.2.1. Heat Transfer

 
1.9.2.1.1. Static Temperature

The static temperature is specified at the supersonic inlet boundary:

(1–225)

 
1.9.2.1.2. Total Temperature

Total temperature is specified at the supersonic inlet boundary:

(1–226)

Static temperature is dynamically computed from the definition of total temperature.