Determine the length of the pipe

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Reference no: EM131369092

Supersonic airflow enters an adiabatic, constant area pipe (inside diameter = 0.1 m) with Ma₁= 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.

Reference no: EM131369092

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