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publishCompany Cambridge University Press
EISBN 9780511217920
PISBN 9780521858106
edition 1
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  • Contents
This book is intended for advanced undergraduate and graduate students in mechanical and aerospace engineering taking a course commonly called Principles of Turbomachinery or Aerospace Propulsion. It begins with a review of basic thermodynamics and fluid mechanics principles to motivate their application to aerothermodynamics and real-life design issues. This approach is ideal for the reader who will face practical situations and design decisions in the gas turbine industry. Among the features of the book are: • An emphasis on the role of entropy in assessing machine performance • A timely review of flow structures • Revisiting the subsonic and supersonic De Laval nozzle as it applies to bladed turbomachinery components • An applied review of boundary layer principles • And highlighting the importance of invariant properties across a turbomachinery component in carrying out real computational tasks. The text is fully supported by over two hundred figures, numerous examples and homework problems.
    Collected by
    • UCLA
    • The British Library
    • Yale University
    • University of Cambridge
    • Princeton University
    • University of Oxford
    • Harvard University
    • University of Melbourne Library
    • Columbia University Library
    • Stanford University
    • MIT
    • UCB

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