Thermodynamics: An Engineering Approach 8th Edition

Published by McGraw-Hill Education
ISBN 10: 0-07339-817-9
ISBN 13: 978-0-07339-817-4

Chapter 17 - Compressible Flow - Problems - Page 893: 17-101C

Answer

See explanation

Work Step by Step

In Rayleigh flow, the stagnation temperature $T_{0}$ always increases with heat transfer to the fluid, but the temperature T decreases with heat transfer in the Mach number range of $0.845 < Ma < 1$ for air. Therefore, the temperature in this case will decrease.
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