Consider an oblique shock wave with (M_{1}=4.0) and (beta=50^{circ}). This shock wave is incident on a constant-pressure

Question:

Consider an oblique shock wave with $M_{1}=4.0$ and $\beta=50^{\circ}$. This shock wave is incident on a constant-pressure boundary, as sketched in Fig. 5.26. For the flow downstream of the reflected expansion wave, calculate the Mach number $M_{3}$ and the flow direction relative to the flow upstream of the shock.

Figure 5.26:

image text in transcribed