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| Aerothermodynamics of Gas Turbine and Rocket Propulsion |
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Gordon C. Oates
AIAA Education Series
Published by AIAA, © 1997, 3rd Edition, 452 pages, Mixed media
ISBN-10: 1-56347-241-4
ISBN-13: 978-1-56347-241-1
Download Supporting Materials
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AIAA Member Price:
$59.95
List Price:
$84.95
AIAA Members Save 29%!
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Best Seller! Winner of the Summerfield Book Award. This seminal book on gas turbine technology has been a best-seller 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, 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 386 (compatible) or higher, 8 Mb RAM, 20 Mb of available disk space.
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Table of Contents:
- Thermodynamics and Quasi-One-Dimensional Fluid Flows
- Chemical Rockets
- Nonchemical Rockets
- Ideal Cycle Analysis
- Component Performance
- Nonideal Cycle Analysis
- Engine Off-Design Performance
- Elementary Theory of Blade Aerodynamics
- Throughflow Theory
- Cascade Flows
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