Find the mach number and the stagnation temperature

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Reference no: EM131238493

1. A jet flies at an altitude of 12 km where the air is at -40?C, 45 kPa, with a velocity of 1000 km/h. Find the Mach number and the stagnation temperature on the nose.

2. The speed of sound in liquid water at 25?C is about 1500 m/s. Find the stagnation pressure and temperature for a M = 0.1 flow at 25?C, 100 kPa. Is it possible to get a significant Mach number flow of liquid water?

Reference no: EM131238493

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