12.21 Air at a pressure and temperature of 100 in. of mercury absolute and 100 F, respectively,...
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12.21 Air at a pressure and temperature of 100 in. of mercury absolute and 100 F, respectively, discharges at a rate of 5 lbm/s from a tank through a convergent-divergent nozzle into another tank maintained at a pressure of 20 in. of mercury. Determine the nozzle throat and exit diameters for full expansion. Determine the pressure, temperature, velocity in the throat, and the Mach number at the nozzle exit.
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Related Book For
Fox And McDonald S Introduction To Fluid Mechanics
ISBN: 9781119721024
10th Edition
Authors: Robert W. Fox, Alan T. McDonald, John W. Mitchell
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