Calculate mach number upstream of the shock


Upstream of a normal shock in air the pressure is 14.7 psia and the temperature is 528R. Downstream of the shock the air pressure is 76.8 psia. What is the Mach number upstream of the shock? What is the Mach number downstream of the shock? What is the temperature downstream of the shock. What is the change in entropy across the shock?

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Physics: Calculate mach number upstream of the shock
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