Air enters a 5.5-cm-diameter adiabatic duct with inlet conditions of (mathrm{Ma}_{1}=2.2, T_{1}=250 mathrm{~K}), and (P_{1}=60 mathrm{kPa}), and
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Air enters a 5.5-cm-diameter adiabatic duct with inlet conditions of \(\mathrm{Ma}_{1}=2.2, T_{1}=250 \mathrm{~K}\), and \(P_{1}=60 \mathrm{kPa}\), and exits at a Mach number of \(\mathrm{Ma}_{2}=1.8\). Taking the average friction factor to be 0.03 , determine the velocity, temperature, and pressure at the exit.
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Solution To solve this problem well use the equations for compressible flow in a duct including the conservation of mass momentum and energy as well a...View the full answer
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Related Book For 
Fluid Mechanics Fundamentals And Applications In SI Units
ISBN: 9789814821599
4th Edition
Authors: Yunus Cengel, John Cimbala
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