Chapter 9, Problem 9.9P

Consider an oblique shock generated at a compression corner with a deflection angle $\theta =\text{18}.\text{2}°$. A straight horizontal wall is present above the corner, as shown in Figure 9.19. If the upstream flow has the properties $M_1=\text{3}.\text{2},P_1=\text{1 atm}$ and $T_1=\text{52}0°\text{R}$, calculate $M_3,p_3,$ and $T_3$ behind the reflected shock from the upper wall. Also, obtain the angle $\Phi$ which the reflected shock makes with the upper wall.