Consider supersonic airflow through a 12-cm- diameter
Chapter 12, Problem 153P(choose chapter or problem)
Problem 153P
Consider supersonic airflow through a 12-cm- diameter adiabatic duct with inlet conditions of T1 = 530k, P1 = 80 kPa. and Ma1 = 3. Taking the average friction factor to be 0.03, determine the duct length required to accelerate the flow to a Mach number of unity. Also, calculate the duct length at Mach number for 1 ≤ Ma ≤ 3. Discuss the result.
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