**
Given the initial conditions:
- Total temperature, \( T_0 = 293 \, \text{K} \)
- Total pressure, \( p_0 = 101 \, \text{kPa} \)
- Mach number at section 1, \( \text{Ma}_1 = 0.2 \)
Since the gas is helium, we will use its specific heat capacities:
- \(
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