A converging–diverging nozzle receives air from a tank at 100 psia and 600°R. The pressure is 28.0 psia immediately preceding a plane shock that is located in the di- verging section. The Mach number at the exit is 0.5 and the flow rate is 10 lbm/sec. Determine: (a) The throat area. (b) The area at which the shock is located. (c) The outlet pressure required to operate the nozzle in the manner described abov

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