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An aeroplane is cruising at a speed of 800 kmph at an altitude, where the air temperature is 0°C. The flight Mach number at this speed is nearly,
  • a)
    1.5
  • b)
    0.254
  • c)
    0.67
  • d)
    2.04
Correct answer is option 'C'. Can you explain this answer?
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An aeroplane is cruising at a speed of 800 kmph at an altitude, where ...
°C. Due to a mechanical failure, the plane loses altitude and descends to an altitude where the air temperature is -10°C. Assuming that the pressure remains constant, what is the change in airspeed of the plane as it descends?
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