Question: Supersonic flow inside a duct encounters a sharp step, leading to shock formation. Determine the Mach number, pressure, and temperature right after the shock for

Supersonic flow inside a duct encounters a sharp step, leading to shock formation. Determine the Mach number, pressure, and temperature right after the shock for each zone (in terms of incoming flow properties). You may need to have the shock angle in the zone (3) as 45
Supersonic flow inside a duct encounters a sharp

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