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Engineering, 20.02.2020 05:38, maariaaa10
At a given point in a supersonic wind tunnel, the pressure and temperature are 5×104 N/m2 and 200 K, respectively. The total pressure at this point is 1.5×106 N/m2. Calculate the local Mach number and total temperature.
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At a given point in a supersonic wind tunnel, the pressure and temperature are 5×104 N/m2 and 200 K,...
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