Answer Happy

Part B: An incident oblique shock wave strikes a solid wall exactly in the corner of an expansion corner at an angle-of-incidence to the wall of di = 30° as seen in the attached Figure Two. As the flow passes through the incident shock from Region One to Region Two, the flow is turned (deflected) through an angle 102 = 15.7844789 degrees. The Mach number in Region Three is equal to that in Region One (M1=M3). Determine: f) M, M2 M3 Mach number in Regions One, Two, and Three (5 points) g) 203 flow turning, i.e. flow deflection angle as the flow turns away from itself in the expansion from Region Two to Region Three (5 points) h) The wall angle ß defined in Figure Two. (5 points) Note For full credit on this problem, at least 6 digits of accuracy should be carried throughout all the calculations, and results must be reported with at least four significant digits. (For numbers having an absolute value less than one, leading zeros after the decimal do not count.)
Генератар Fan / / Moo = ? M, = 5.57428061 P/P = 0.2869401635 oblique 8) 0 slip line (2 UN 빠 oblique M2 = 3.65083126 P/P = 2.76417243 Shock 2 expansion fan