A highspeed aircraft is flying at an elevation of 8000 ft Th

A high-speed aircraft is flying at an elevation of 8.000 ft. The plane is heard 12 s after the sound was emitted. The air temperature is 20degree F. Determine the Mach number and the speed of the aircraft in mph. Gas constant R = 1716 (ft-lbf)/(slug-degreeR).

Solution

Speed of sound c = [k R T]1/2= [ 1.4 (1716 ft lb/slug oR) ((20 oF) + (460 oR)) ]1/2   = 1073.84 ft/s

Speed of aircraft = 8000/12 = 666.67 ft/s

Mach Number = Speed of aircraft / Speed of sound

= 1073.84 / 666.67

= 1.61

So, the speed is supersonic

 A high-speed aircraft is flying at an elevation of 8.000 ft. The plane is heard 12 s after the sound was emitted. The air temperature is 20degree F. Determine

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