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:

Transcribed Image Text:

Constant poo Incident shock Reflected expansion