Air at 200 kPa, 100C, and Mach number Ma = 0.8 flows through a duct. Find the

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Air at 200 kPa, 100°C, and Mach number Ma = 0.8 flows through a duct. Find the velocity and the stagnation pressure, temperature, and density of the air.
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Thermodynamics An Engineering Approach

ISBN: 978-0073398174

8th edition

Authors: Yunus A. Cengel, Michael A. Boles

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