Consider the isentropic subsonic-supersonic flow through a convergent-divergent nozzle. The reservoir pressure and temperature are \(10 \mathrm{~atm}\) and \(300 \mathrm{~K}\), respectively. There are two locations in the nozzle where \(A / A^{*}=6\) : one in the convergent section and the other in the divergent section. At each location, calculate \(M, p, T\), and \(u\).