Compressible Flow
An ideal gas flows through a duct. At a particular location, the temperature, pressure, and velocity are known. Determine the Mach number, stagnation temperature, in °R, and the stagnation pressure, in lbf/in.2, for
(a) air at 310°F, 100 lbf/in.2, and a velocity of 1400 ft/s.
(b) helium at 520°R, 20 lbf/in.2, and a velocity of 900 ft/s.
(c) nitrogen at 600°R, 50 lbf/in.2, and a velocity of 500 ft/s.
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