Engineering, 21.02.2020 03:58, hipeopleitsme121

At a given point in a supersonic wind tunnel, the pressure and temperature are 5×10^4 N/m^2 and 200 K, respectively. The total pressure at this point is 1.5×106 N/m^2. 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 5×10^4 N/m^2 and 200...