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Jet Propulsion: A Simple Guide to the Aerodynamic and Thermodynamic Design and Performance of Jet Engines (Cambridge Engine Technology Series)
 
 
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Jet Propulsion: A Simple Guide to the Aerodynamic and Thermodynamic Design and Performance of Jet Engines (Cambridge Engine Technology Series) [Paperback]

Nicholas A. Cumpsty (Author)
4.3 out of 5 stars  See all reviews (3 customer reviews)


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Paperback $62.68  
Paperback, January 28, 1998 --  
There is a newer edition of this item:
Jet Propulsion: A Simple Guide to the Aerodynamic and Thermodynamic Design and Performance of Jet Engines Jet Propulsion: A Simple Guide to the Aerodynamic and Thermodynamic Design and Performance of Jet Engines 4.3 out of 5 stars (3)
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Book Description

January 28, 1998 0521596742 978-0521596749
This text provides a 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, as well as off-design performance. Although the book assumes familiarity with basic fluid mechanical ideas, background is given where necessary. The book emphasises principles and ideas, with simplification and approximation used where this helps understanding. Many exercises (using numerical rather than algebraic solutions, with realistic empirical input where needed) support and reinforce the text. A detailed glossary is included. This text is suitable for student courses in aircraft propulsion and jet engine design, but will be invaluable as a guide and reference for engineers in the engine and airframe industry.


Editorial Reviews

Review

'I found the book eminently readable, I will find it very helpful and will advocate it to students ... and colleagues. One can think of many other engineering topics that would benefit from books having the lucid style and up-to-the-minute credibility of this well-priced one.' Ray Whitford, Institute of Mechanical Engineering

'As an introductory guide to design, and an indication of why modern engines are 'how they are', this book deserves to be used wherever aircraft propulsion is taught. Like a good jet engine, it has the potential for future development and updating in new versions and should enjoy a long and useful life.' Frank Armstrong, The Aeronautical Journal

Book Description

Through two engine design projects, first for a new large passenger aircraft and second for a new fighter aircraft, this text introduces, illustrates and explains the important facets of modern engine aerothermal design. Principles and ideas are emphasised and many examples and exercises reinforce the text.

Product Details

  • Paperback: 297 pages
  • Publisher: Cambridge University Press (January 28, 1998)
  • Language: English
  • ISBN-10: 0521596742
  • ISBN-13: 978-0521596749
  • Product Dimensions: 9.6 x 6.8 x 0.5 inches
  • Shipping Weight: 1.2 pounds
  • Average Customer Review: 4.3 out of 5 stars  See all reviews (3 customer reviews)
  • Amazon Best Sellers Rank: #3,302,352 in Books (See Top 100 in Books)

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Average Customer Review
4.3 out of 5 stars (3 customer reviews)
 
 
 
 
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29 of 30 people found the following review helpful:
5.0 out of 5 stars Really helpful, September 30, 2000
This review is from: Jet Propulsion: A Simple Guide to the Aerodynamic and Thermodynamic Design and Performance of Jet Engines (Cambridge Engine Technology Series) (Paperback)
This book keeps up with the promise in the title. It is a easily readable guide to design and perfomance of jet engine with a rigorous treatise of each field, even if the level remains simple.

In fact the mathematical exposition is quite accessible, without a full analytical presentation. Nevertheless the formulae are clearly given with an effective theorical background when needed. Since the volume target is to clarify ideas and principles, each topic is attractively examined, emphasizing the qualitative treatment over the quantitative analysis to improve understanding of physical phenomena. This facet is quite useful because it allows an overall comprehension in mastering design process of jet engine. Besides, the emphasis on having a clear picture of principles provides the basis for a fair evaluation of engine perfomances under real conditions.

As a guide or a reference, this work has neatly achived its goal.

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6 of 8 people found the following review helpful:
5.0 out of 5 stars Outstanding Book, April 4, 2007

This is an outstanding book by a knowledgeable author that provides the basic know-how and skills that an aeronautical or mechanical engineer with an interest in jet propulsion will find useful and helpful. The book is well written in a readable and easy to follow format that provides the reader with a comprehensive overview of jet propulsion. The author clearly presents the concepts, principles and design issues of modern gas turbine engines.

The reader will learn the various components of a jet engine including the intake design, compressors, turbines, combustion chamber designs, and the jet pipe and how thrust is produced as well as the physics and thermodynamics that go with these.

The book has great explanations, diagrams and figures that the reader will find useful and helpful. I recommend the book to engineers wishing to learn more about the jet engine.
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0 of 2 people found the following review helpful:
3.0 out of 5 stars Jet Propulsion Books, October 21, 2011
Amazon Verified Purchase(What's this?)
Book is fine, however I ordered on 17 books on September 19. I am still waiting to receive 9. The vendor told me that they would have all books in three weeks. I accepted this statement, understanding that the class that started October 6 would have to wait. Class is over and they are still waiting.
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Inside This Book (learn more)
First Sentence:
This chapter looks at some of the commercial requirements and background to the proposals to build a new civil airliner capable of carrying about 600 people. Read the first page
Key Phrases - Statistically Improbable Phrases (SIPs): (learn more)
compressor delivery temperature, fan pressure ratio, propelling nozzle area, inlet stagnation pressure, rotor cooling air, bet velocity, overall pressure ratio, inlet stagnation temperature, core mass flow, bypass nozzle, gross thrust, core compressor, corrected mass flow, dimensional mass flow, bet pipe, final nozzle, new large aircraft, engine inlet temperature, mixed turbofan, design pressure ratio, stagnation pressure loss, design point operation, civil engine, unburned air, mixed engine
Key Phrases - Capitalized Phrases (CAPs): (learn more)
Rolls Royce, General Electric
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