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1. A high-speed missile is traveling at Mach 3 at standard sea level. What is its velocity in miles per hour? 2. Calculate the flight Mach number for the supersonic transport in Prob. 4.12. 3. Consider a low-speed subsonic wind tunnel with a nozzle contraction ratio of 1 : 20. One side of a mercury manometer is connected to the settling chamber and the other side to the test section. The pressure and temperature in the test section are 1 and 300 K., respectively. What is the height difference between the two columns of mercury when the test section velocity is 80 m/s? Prob. 4.12. A supersonic transport is flying at a velocity of 1500 mi1h at a standard altitude of 50,000 ft. The temperature at a point in the flow over the wing is 793.32°R. Calculate the flow velocity at that point.
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