A normal shock is positioned in the diverging portion of a
Chapter 11, Problem 11.70(choose chapter or problem)
A normal shock is positioned in the diverging portion of a frictionless, adiabatic, converging–diverging airflow duct where the cross-sectional area is \(0.1 ~\mathrm{ft^2}\) and the local Mach number is 2.0. Upstream of the shock, \(p_0= 200 ~\mathrm{psia}\) and \(T_0 =1200\mathrm{ ~^\circ R}\). If the duct exit area is \(0.15~\mathrm{ ft^2}\), determine the exit area temperature and pressure and the duct mass flowrate.
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