A uniform supersonic stream with (M_{1}=1.5, p_{1}=1700 mathrm{lb} / mathrm{ft}^{2}), and (T_{1}=460^{circ} mathrm{R}) encounters an expansion corner

Question:

A uniform supersonic stream with $M_{1}=1.5, p_{1}=1700 \mathrm{lb} / \mathrm{ft}^{2}$, and $T_{1}=460^{\circ} \mathrm{R}$ encounters an expansion corner (see Fig. 4.32) which deflects the stream by an angle $\theta_{2}=20^{\circ}$. Calculate $M_{2}, p_{2}, T_{2}, p_{o_{2}}, T_{o_{2}}$, and the angles the forward and rearward Mach lines make with respect to the upstream flow direction.

Figure 4.32:

image text in transcribed