Air flows through a converging-diverging nozzle that has an area ratio of 3.5. The nozzle is operating at its third critical (design condition). The jet stream strikes a two-dimensional wedge with a total wedge angle of 40 degree as shown in Figure P8.12. Make a sketch to show the initial wave pattern that results from the jet stream striking the wedge. Show the additional wave pattern formed by the interaction of the initial wave system with the free boundary. Mark the flow direction in the region following each wave form and show what happens to the free boundary. Compute the Mach number and direction of flow after the air jet passes through each system of waves.
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