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Aerothermodynamics of Gas Turbine Rocket Propulsion [With *]

AUTHOR G. Oates; Oates, Gordon C.; American Institute of Aeronautics and Astronautics
PUBLISHER AIAA (American Institute of Aeronautics & Ast (01/01/1997)
PRODUCT TYPE Hardcover (Hardcover)

Description
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 Format
Product Details
ISBN-13: 9781563472411
ISBN-10: 1563472414
Content Language: English
Edition Number: 0003
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Page Count: 456
Carton Quantity: 0
Product Dimensions: 6.30 x 1.37 x 9.22 inches
Weight: 1.88 pound(s)
Country of Origin: US
Subject Information
BISAC Categories
Technology & Engineering | Aeronautics & Astronautics
Technology & Engineering | Mechanics - Thermodynamics
Technology & Engineering | Aviation - General
Dewey Decimal: 629.134
Library of Congress Control Number: 97051303
Descriptions, Reviews, Etc.
annotation
This seminal book on gas turbine technology has been a bestseller 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 include atmosphere programs, quasi-one-dimensional flow programs, gas turbine programs, and rocket combustion programs.
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publisher marketing
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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List Price $84.95
Your Price  $84.10
Hardcover