- Textbook
- eCollection
Description
Now in its third edition, Jet Propulsion offers a self-contained introduction to the aerodynamic and thermodynamic design of modern civil and military jet engine design. Through two-engine design projects for a large passenger and a new fighter aircraft, the text explains modern engine design. Individual sections cover aircraft requirements, 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…
- Add bookmark
- Cite
- Share
Key features
- The emphasis is on simple, realistic, design examples of real jet engines, especially engines under development at present - these real examples of current applications of technology give readers additional insight
- Addresses the modern aircraft industry shift to two-engine aircraft with a greater emphasis on reduction of fuel burn; the model created for Part I is the new efficient aircraft, a twin aimed at high efficiency
- Contains a substantial number of exercises, which follow, as far as possible, logical steps in the design of the civil engine and the military combat engine
- Coverage in the third edition switches to using fan pressure ratio as the independent design variable rather than bypass ratio, thus making use of modern state-of-the-art design strategies and giving a much clearer insight into controlling effects
About the book
- DOI https://doi.org/10.1017/CBO9781316223116
- Subjects Aerospace Engineering,Engineering,Thermal-Fluids Engineering
- Format: Paperback
- Publication date: 22 July 2015
- ISBN: 9781107511224
- Dimensions (mm): 247 x 174 mm
- Weight: 0.71kg
- Contains: 124 b/w illus. 29 tables 141 exercises
- Page extent: 365 pages
- Availability: In stock
- Format: Digital
- Publication date: 28 May 2018
- ISBN: 9781316223116
Access options
Check your access to the full version of this content by using one of the options below
If you should have access and can't see this content please contact customer support