Jet Propulsion - Nicholas Cumpsty

Jet Propulsion

A Simple Guide to the Aerodynamic and Thermodynamic Design and Performance of Jet Engines
Buch | Softcover
318 Seiten
2003 | 2nd Revised edition
Cambridge University Press (Verlag)
978-0-521-54144-2 (ISBN)
68,55 inkl. MwSt
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The second edition of Cumpsty's excellent self-contained introduction to aerodynamic and thermodynamic design of modern civil and military jet engines. Throughly updated and revised, including a new appendix on noise control and expanded treatment of emissions. Suitable for student courses in aircraft propulsion, and an invaluable reference for aerospace engineers.
This is the second edition of Cumpsty's excellent self-contained introduction to the aerodynamic and thermodynamic design of modern civil and military jet engines. Through two engine design projects, first for a new large passenger aircraft, and second for a new fighter aircraft, the text introduces, illustrates and explains the important facets of modern engine design. Individual sections cover aircraft requirements and aerodynamics, principles of gas turbines and jet engines, elementary compressible fluid mechanics, bypass ratio selection, scaling and dimensional analysis, turbine and compressor design and characteristics, design optimization, and off-design performance. The book emphasises principles and ideas, with simplification and approximation used where this helps understanding. This edition has been thoroughly updated and revised, and includes a new appendix on noise control and an expanded treatment of combustion emissions. Suitable for student courses in aircraft propulsion, but also an invaluable reference for engineers in the engine and airframe industry.

Nicholas Cumpsty is Professor of Aerothermal Technology at the University of Cambridge. He is a Fellow of the Royal Academy of Engineering and of the Institution of Mechanical Engineers. He is also a Fellow of both the American Society of Mechanical Engineers and of the American Institute of Aeronautics and Astronautics.

Part I. Design of Engines for a New 600-Seat Aircraft: 1. Introduction; 2. The aerodynamics of the aircraft; 3. The creation of thrust in the engine; 4. The gas turbine cycle; 5. The principle and layout of jet engines; 6. Elementary fluid mechanics of compressible gases; 7. The selection of bypass ratio; 8. Dynamic scaling and dimensional analysis; 9. Turbomachinery: turbines and compressors; 10. Overview; Part II. Engine Component Characteristic and Engine Matching: 11. Component characteristics; 12. Engine matching off-design; Part III. The Design of the Engines for a New Fighter Aircraft: 13. A new fighter aircraft; 14. Lift, drag and the effects of manoeuvring; 15. Engines for combat aircraft; 16. Design point for a combat aircraft; 17. Combat engines off-design; 18. Turbomachinery for combat aircraft; Part IV. A Return to the Civil Engine: 19. A return to the civil transport engine; 20. Conclusion; Appendix: Jet engine noise control; Bibliography; Index.

Erscheint lt. Verlag 14.8.2003
Zusatzinfo 3 Halftones, unspecified; 140 Line drawings, unspecified
Verlagsort Cambridge
Sprache englisch
Maße 175 x 247 mm
Gewicht 640 g
Themenwelt Technik Fahrzeugbau / Schiffbau
Technik Luft- / Raumfahrttechnik
Technik Maschinenbau
ISBN-10 0-521-54144-1 / 0521541441
ISBN-13 978-0-521-54144-2 / 9780521541442
Zustand Neuware
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