**
Given:
- Temperature, \( T_1 = 20^{\circ} \mathrm{C} = 293.15 \, \mathrm{K} \)
- Pressure, \( p_1 = 300 \, \mathrm{kPa} \)
Using the ideal gas law, we can find the density of air at the inlet:
\[
R = 287 \, \mathrm{J/(kg \cdot K)} \quad
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