Calculate the local mach number and total temperature


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

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Mechanical Engineering: Calculate the local mach number and total temperature
Reference No:- TGS0834254

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