Solved: Air at 200 kPa, 100°C, and Mach number Ma = 0.8
Chapter 12, Problem 25P(choose chapter or problem)
Problem 25P
Air at 200 kPa, 100°C, and Mach number Ma = 0.8 flows through a duct. Calculate the velocity and the stagnation pressure, temperature, and density of the air.
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