Compute the mass flow-shock


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Q: Air flows through a duct as in Fig, 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.

197_Normal shock.jpg

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Mechanical Engineering: Compute the mass flow-shock
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