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17- Air flows isentropically through a c-d nozzle at a rate of 1.2kg//s from a large reservoir in which the temperature is 310K. At the
17- Air flows isentropically through a c-d nozzle at a rate of 1.2kg//s from a large reservoir in which the temperature is 310K. At the nozzle exit, the pressure is to be 14kPa and the Mach number is 2.4 . Find: (1) The pressures at the reservoir and at the throat (2) The throat and exit areas of the nozzle
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