Part A: An incident oblique shock wave strikes a solid wall exactly in the corner of a compression wedge at an angle-of-

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Part A An Incident Oblique Shock Wave Strikes A Solid Wall Exactly In The Corner Of A Compression Wedge At An Angle Of 1 (201.05 KiB) Viewed 22 times

Part A An Incident Oblique Shock Wave Strikes A Solid Wall Exactly In The Corner Of A Compression Wedge At An Angle Of 2 (179.69 KiB) Viewed 22 times

Part A: An incident oblique shock wave strikes a solid wall exactly in the corner of a compression wedge at an angle-of-incidence to the wall of Qı = 30° as seen in the attached Figure One. The static pressure ratio across the incident shock is P2/P1 = 3.40625, and the Mach number in Region Three is M3 = 1.0. Determine: a) M Mach number in Region One (5 points) b) 102 flow turning, i.e. flow deflection angle from Region One to Region Two (5 points) c) M2 Mach number in Region Two (5 points) d) 203 flow turning, i.e. flow deflection angle from Region Two to Region Three (5 points) e) The wall angle B defined in Figure One. (5 points)
3 .Compression Corner Solid Wall سر سے / کر Solid Wall Opa B=? (Determin.) O ck=30 3 M,=? (Determine) M = ? M₂=1.0 ed/a- - (determine) 3.40625000 incident Shock reflected Shock