Air enters a 5.5-cm-diameter adiabatic duct with inlet conditions of Ma 1 = 2.2, T 1 = 250 K, and
Air enters a 5.5-cm-diameter adiabatic duct with inlet conditions of Ma1 = 2.2, T1 = 250 K, and P1 = 70 kPa, and exits at a Mach number of Ma2 = 1.8. Taking the average friction factor to be 0.03, determine the velocity, temperature, and pressure at the exit.
To determine the velocity temperature and pressure at the exit of the duct we can use the following steps Calculate the area of the duct A d 2 2 5 5 c…View the full answer
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