Consider air flowing in a divergent duct with an inlet Mach number of 0.2, with an area 7 ft2 and temeprature of 520 R. If the area at the exit is 16 ft2, what is the velocity of the air at the point? Assume k is 1.14 and R is 1716 ft lb/slug R.
Consider air flowing in a divergent duct with an inlet Mach number of 0.2, with an area 7 ft2 and temeprature of 520 R. If the area at the exit is 16 ft2, what is the velocity of the air at the point? Assume k is 1.14 and R is 1716 ft lb/slug R.