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Aerothermodynamics of Gas Turbine Rocket Propulsion [With *]
 
 

Aerothermodynamics of Gas Turbine Rocket Propulsion [With *] [Hardcover]

Gordon C. Oates , G. Oates

List Price: CDN$ 86.62
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Book Description

Includes software

This seminal book on gas turbine technology has been a best-seller since it was first published in 1984. It now includes a comprehensive set of software programs that complement the text with problems and design analyses. Software topics included are: atmosphere programs, quasi-one-dimensional flows programs (ideal constant-area heat interaction, adiabatic constant-area flow with friction, rocket nozzle performance, normal shock waves, oblique shock waves), gas turbine programs (engine cycle analysis and engine off-design performance), and rocket combustion programs (Tc and Pc given, Hc and Pc given, isentropic expansion). Used as a standard text in more than 50 universities, the book and software will continue to fulfill the need for a comprehensive modern book on the principles of propulsion.

System Requirements:IBM PC 386/486/586/Pentium or compatible; 640 Kb RAM hard disk with 1.0 Mb of available disk space; EGA or better video capability


Inside This Book (Learn More)
First Sentence
The propulsion provided by airbreathing and rocket engines is basically similar in that thrust is obtained by generating rearward momentum in one or more streams of gas. Read the first page
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Front Cover | Copyright | Table of Contents | Excerpt | Index | Back Cover
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Amazon.com: 5.0 out of 5 stars (1 customer review)

5.0 out of 5 stars Great book!, Oct 9 2011
By trzachar - Published on Amazon.com
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This review is from: Aerothermodynamics of Gas Turbine Rocket Propulsion [With *] (Hardcover)
This is a great book for learning about gas turbines and rocket engines. Discusses the aerothermodynamics behind the engines. Overall great book!
 Go to Amazon.com to see the review  5.0 out of 5 stars 

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