Air flows through a duct as in Fig P9.84, where A1 = 24 cm2, A2 = 18

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Air flows through a duct as in Fig P9.84, where A1 = 24 cm2, A2 = 18 cm2, and A3 = 32 cm2. A normal shock stands at section 2. Compute
(a) The mass flow,
(b) The Mach number, and
(c) The stagnation pressure at section 3.

Air flows through a duct as in Fig P9.84
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