A shock stands at the inlet to the system shown in fig The f

A shock stands at the inlet to the system shown in fig. The free - stream Mach number is M = 2.90 the fluid is nitrogen, A_2 = 0.205 m^2, A_3 = 0.2 m^2. Find the outlet Mach number is M Find the outlet Mach number and the temperature ratio T_3 / T_1

Solution

M₂=0.48137956

T₃/T₁=2.56320749