Aerothermodynamics of Gas Turbine and Rocket Propulsion

Aerothermodynamics of Gas Turbine and Rocket Propulsion - AIAA Education Series

Revised and enl

Paperback (30 Jun 1996)

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Publisher's Synopsis

This text on gas turbine technology has been a best-seller since it was first published in 1984. This revised edition now includes a comprehensive set of software programmes that complement the text with problems and design analyses. Software topics included are: atmosphere programmes, quasi-1D flows programmes (ideal constant-area heat interaction, adiabatic constant-area flow with friction, rocket nozzle performance, normal shock waves, oblique shock waves), gas turbine programmes (engine cycle analysis and engine off-design performance), and rocket combustion (tc and pc are given, hc and pc are given, Isentropic expansion). Used as a standard text in more than 50 universities, the book and software continue to fulfil the need for a comprehensive, modern book on the principles of propulsion. System requirements: IBM PC 386/486/586/Pentium or clone; 640 Kb RAM hard disk with 1.0Mb of available disk space; EGA or better video capability.

Book information

ISBN: 9780930403348
Publisher: American Institute of Aeronautics & Astronautics
Imprint: AIAA
Pub date:
Edition: Revised and enl
DEWEY: 629.12
DEWEY edition: 19
Language: English
Number of pages: 452
Weight: -1g
Height: 230mm