Compressible Flow Air at po = 1.4 bar, To = 280 K expands isentropically through a converging nozzle and discharges to the atmosphere at 1 bar. The exit plane area is 0.0013 m2.
(a) Determine the mass flow rate, in kg/s.
(b) If the supply region pressure, po, were increased to 2 bar, what would be the mass flow rate, in kg/s?
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