12.22 Air flows adiabatically through a duct. At the entrance, the static temperature and pressure are 310

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12.22 Air flows adiabatically through a duct. At the entrance, the static temperature and pressure are 310 K and 200 kPa, respectively.

At the exit, the static and stagnation temperatures are 294 K and 316 K, respectively, and the static pressure is 125 kPa. Find

(a) the Mach numbers of the flow at the entrance and exit and

(b) the area ratio A2/A1.

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