Supersonic airflow enters an adiabatic, constant area (insidediameter = 1 ft) 30-ft-long
Chapter 11, Problem 11.58(choose chapter or problem)
Supersonic airflow enters an adiabatic, constant area (insidediameter = 1 ft) 30-ft-long pipe with Ma1 = 3.0. The pipe frictionfactor is estimated to be 0.02. What ratio of pipe exit pressure topipe inlet stagnation pressure would result in a normal shock wavestanding at (a) x = 5 ft, or (b) x = 10 ft, where x is the distancedownstream from the pipe entrance? Determine also the duct exitMach number and sketch the temperatureentropy diagram foreach situation
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