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 9 - Gas Power Cycles - Problems - Page 546: 9-128C

Answer

See explanation below.

Work Step by Step

The effect of turbine and compressor irreversibilities of a turbojet engine reduced the exit velocity of the vehicle. Hence it will reduce the thrust.
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