Carbon dioxide enters converging-diverging nozzle at 900 kPa and 900 K with a negligible velocity. The flow

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Carbon dioxide enters converging-diverging nozzle at 900 kPa and 900 K with a negligible velocity. The flow is steady and isentropic. For a exit Mach number of 2.5 and a throat area of 25 cm2, determine
(a) The exit area,
(b) The exit velocity.
(c) Mass flow rate () and
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