Supersonic airflow enters an adiabatic, constant area pipe (inside diameter (=0.1 mathrm{~m}) ) with (mathrm{Ma}_{1}=2.0). The pipe
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Supersonic airflow enters an adiabatic, constant area pipe (inside diameter \(=0.1 \mathrm{~m}\) ) 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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Related Book For
Munson Young And Okiishi's Fundamentals Of Fluid Mechanics
ISBN: 9781119080701
8th Edition
Authors: Philip M. Gerhart, Andrew L. Gerhart, John I. Hochstein
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