Consider the flow past a \(30^{\circ}\) expansion corner, as sketched in Fig. 4.32. The upstream conditions are \(M_{1}=2, p_{1}=3 \mathrm{~atm}\), and \(T_{1}=400 \mathrm{~K}\). Calculate the following downstream conditions: \(M_{2}, p_{2}, T_{2}, T_{o_{2}}\), and \(p_{o_{2}}\).

Figure 4.32:

Transcribed Image Text:

M > 1 Pi T Forward Mach line Rearward Mach line M2 P2