Consider an oblique shock generated at a compression corner with a deflection angle = 18.2. A

Consider an oblique shock generated at a compression corner with a deflection angle θ = 18.2°. A straight horizontal wall is present above the corner, as shown in Fig. 9.14. If the upstream flow has the properties M1 = 3.2, p1 = 1atm and T1, = 520°R, calculate M3, p3, and T3 behind the reflected shock from the upper wall. Also, obtain the angle Φ which the reflected shock makes with the upper wall.