Consider a point in a supersonic flow where the static pressure is (0.4 mathrm{~atm}). When a Pitot
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Consider a point in a supersonic flow where the static pressure is \(0.4 \mathrm{~atm}\). When a Pitot tube is inserted in the flow at this point, the pressure measured by the Pitot tube is \(3 \mathrm{~atm}\). Calculate the Mach number at this point.
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