Air flowing at 32 kPa, 240 K, and Ma1 5 3.6 is forced to
Chapter 17, Problem 1790(choose chapter or problem)
Air flowing at 32 kPa, 240 K, and Ma1 5 3.6 is forced to undergo an expansion turn of 158. Determine the Mach number, pressure, and temperature of air after the expansion
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