| Management number | 231722815 | Release Date | 2026/06/18 | List Price | $35.71 | Model Number | 231722815 | ||
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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. Read more
| ASIN | B000TU06YG |
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| XRay | Not Enabled |
| ISBN13 | 978-0511363429 |
| Edition | 1st |
| Language | English |
| File size | 12.8 MB |
| Page Flip | Not Enabled |
| Publisher | Cambridge University Press |
| Word Wise | Not Enabled |
| Print length | 600 pages |
| Accessibility | Learn more |
| Part of series | Cambridge Aerospace |
| Publication date | July 31, 2006 |
| Enhanced typesetting | Not Enabled |
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