Air flowing at 40 kPa, 210 K, and a Mach number of 3 4 impinges on a two dimensional wedge of half angle 8 Determine the two possible oblique shock angles, weak and strong , that could be formed by this wedge For each case, calculate the pressure and Mach number downstream of the oblique shock ...

Air flowing at a specified supersonic Mach number impinges on a twodimensional wedge The shock angle ...

Air flowing at 40 kPa, 210 K, and a Mach number of 3.4 impinges on a two-dimensional

Question:

Air flowing at 40 kPa, 210 K, and a Mach number of 3.4 impinges on a two-dimensional wedge of half-angle 8°. Determine the two possible oblique shock angles, β_weak and β_strong, that could be formed by this wedge. For each case, calculate the pressure and Mach number downstream of the oblique shock.

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