ENGINEERINGThe flow just upstream of a normal shock wave is given by $p_1 = 1 atm, T_1 = 288 K,$ and $M_1 = 2.6.$ Calculate the following properties just downstream of the shock: $p_2, T_2,
ho_2, M_2, p_0, 2, T_0,2,$ and the change in entropy across the shock.