Supersonic air at Mach 3 and 75 kPa impinges on a two dimensional wedge of half angle

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Supersonic air at Mach 3 and 75 kPa impinges on a two dimensional wedge of half angle 10o. Determine
(a) The Mach number downstream of the oblique shock for each case.
(b) The pressure downstream of the oblique shock for each case and
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