ENGLISH

Aerothermodynamics of Gas Turbine and Rocket Propulsion

By Oates , Gordon C.

Book information

Publisher
American Institute of Aeronautics and Astronautics
Year
1997
ISBN
978-1-60119-222-6, 978-1-56347-241-1
Language
english
Format
PDF
Filesize
7 MB (7130482 bytes)
Edition
3rd Edition
Pages
456\499
Orientation
yes
Scanned
landscape
Time added
2013-08-14 18:00:00

Description

This 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). - Data and information appearing in this book are for informational purposes only. AIAA and the author are not responsible for any injury or damage resulting from use or reliance, nor do AIAA and the author warrant that use or reliance will be free from privately owned rights.

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