Question: Air enters a diffuser at 2 7 C and 1 0 0 kPa . The approach velocity is 3 3 3 m / s .
Air enters a diffuser at C and kPa The approach velocity is m s Assume the flow process to be isentropic If the air velocity leaving the diffuser is m s calculate the entrance and exit Mach numbers the exit static pressure and the percentage change in cross sectional area between entrance and exit sections Does the area increase or decrease?
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