### 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:

| (1–221)

##### 1.9.2.1.2. Total Temperature

Total temperature is specified at the supersonic inlet boundary:

| (1–222)

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

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