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Science/Engineering Aerothermodynamics of Gas Turbine Rocket Propulsion, Third Edition

Posted on 2010-03-16




Name:Science/Engineering Aerothermodynamics of Gas Turbine Rocket Propulsion, Third Edition
ASIN/ISBN:1563472414
Language:English
File size:6.8 Mb
Publisher: AIAA
ISBN: 1563472414
Publish Date: edition 1997
File Type: PDF
Pages: 459 pages
File Size: 6,8 mb
   Science/Engineering Aerothermodynamics of Gas Turbine Rocket Propulsion, Third Edition

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Aerothermodynamics of Gas Turbine Rocket Propulsion, Third Edition

This seminal book on gas turbine technology has been a best-seller 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 included are: atmosphere programs, quasi-one-dimensional flows 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.

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