Supersonic airflow enters an adiabatic, constant area pipe
Chapter 11, Problem 11.72(choose chapter or problem)
Supersonic airflow enters an adiabatic, constant area pipe (inside diameter = 0.1 m) with \(\mathrm{Ma_1 = 2.0}\). The pipe friction factor is 0.02. If a standing normal shock is located right at the pipe exit, and the Mach number just upstream of the shock is 1.2, determine the length of the pipe.
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