Question: Air flows isentropically in a converging-diverging nozzle with a throat area of 3 cm2. At section 1, the pressure is 101 kPa, T1 = 300
(a) Is the nozzle choked? Determine
(b) A1; and
(c) The mass flow. Suppose, without changing stagnation conditions of A1, the flexible throat is reduced to 2 cm2. Assuming shock-free flow, will there be any changes in the gas properties at section 1? If so, calculate the new p1, V1, and T1 and explain.
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Check the Mach number If choked calculate the mass flow May 2 V A 868 1428730... View full answer
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