The reservoir pressure of a supersonic wind tunnel is (10 mathrm{~atm}). A Pitot tube inserted in the
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The reservoir pressure of a supersonic wind tunnel is \(10 \mathrm{~atm}\). A Pitot tube inserted in the test section measures a pressure of \(0.627 \mathrm{~atm}\). Calculate the test section Mach number and area ratio.
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