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Aerothermodynamics of Gas Turbine and Rocket Propulsion (Dias y Dias de Poesia)
 
 
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Aerothermodynamics of Gas Turbine and Rocket Propulsion (Dias y Dias de Poesia) [Hardcover]

G. Oates (Author)
5.0 out of 5 stars  See all reviews (1 customer review)

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Book Description

1563472414 978-1563472411 January 1, 1997 3rd
This seminal book on gas turbine technology has been a bestseller since it was first published. 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 flow 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, He and PC given, isentropic expansion).

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Product Details

  • Hardcover: 452 pages
  • Publisher: AIAA; 3rd edition (January 1, 1997)
  • Language: English
  • ISBN-10: 1563472414
  • ISBN-13: 978-1563472411
  • Product Dimensions: 9.2 x 6.3 x 1.4 inches
  • Shipping Weight: 2.2 pounds (View shipping rates and policies)
  • Average Customer Review: 5.0 out of 5 stars  See all reviews (1 customer review)
  • Amazon Best Sellers Rank: #689,715 in Books (See Top 100 in Books)

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5.0 out of 5 stars Great book!, October 9, 2011
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This review is from: Aerothermodynamics of Gas Turbine and Rocket Propulsion (Dias y Dias de Poesia) (Hardcover)
This is a great book for learning about gas turbines and rocket engines. Discusses the aerothermodynamics behind the engines. Overall great book!
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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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