Upstream of the throat of an isentropic converging
Chapter 11, Problem 11.44(choose chapter or problem)
Upstream of the throat of an isentropic converging–diverging nozzle at section (1), \(V_1 =150~ \mathrm{m/s}\), \(p_1 = 100 \text{ kPa(abs)}\), and \(T_1 = 20^\circ\mathrm{ C}\). If the discharge flow is supersonic and the throat area is \(0.1~\mathrm{ m^2}\), determine the mass flowrate in kg/s for the flow of air.
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