A parallel uniform flow at Mach 2.0 approaches a sharp corner that turns the flow in the clockwise direction by 10.37◦. First calculate the flow Mach number downstream of the expansion corner. Second,...

A parallel uniform flow at Mach 2.0 approaches a sharp corner that turns the flow in the clockwise direction by 10.37◦. First calculate the flow Mach number downstream of the expansion corner. Second, calculate the coordinates of the bending streamline with h₁
= 3.0 and graph the streamline. Assume that the flow is planar 2-D with γ = 1.4.