The stagnation pressure and temperature of air flowing
Chapter 11, Problem 11.37(choose chapter or problem)
The stagnation pressure and temperature of air flowing past a probe are 120 kPa(abs) and \(\mathrm{100~^\circ C}\), respectively. The air pressure is 80 kPa(abs). Determine the airspeed and the Mach number considering the flow to be (a) incompressible, (b) compressible.
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