Question: 1 1 . 6 . 1 WP The stagnation pressure and temperature of air flowing past a probe are 1 2 0 kPa ( ?

11.6.1 WP The stagnation pressure and temperature of air flowing past a probe are 120kPa(?abs) and 100C, respectively. The air pressure is 80kPa(?abs). Determine the airspeed and the Mach number considering the flow to be (a) incompressible, (b) compressible.
1 1 . 6 . 1 WP The stagnation pressure and

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