2. Shock intersection Consider a uniform flow of air at M = 3.0 that enters a channel defined by two sharp wedges with angles as shown in the schematic, Fig. 2. The attached shocks that are generated intersect at C. Due to the asymmetry, a slip line CD inclined at an angle & relative to the incoming stream is formed [10 pts] Determine M2, P2/p and M3, P3/P1 b. [5 pts] Determine M4 and M5. c. [5 pts] Determine . Show your steps clearly. The gas constant for air is R = 287 J/(kg.K) and the specific heat ratio is y = 1.4. Assume that the flow is inviscid. 02 = 12 A M1 = 3.0 2 B C 3 5 E D 03 - = 6 Figure 2-1. Schematic of problem statement (not to scale).