Get Ebooks Aerothermodynamics Of Gas Turbine And Rocket Propulsion (AIAA Education Series)
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.
Hardcover: 452 pages
Publisher: American Institute of Aeronautics and Astronautics; Revised & enlarged edition (October 1987)
Language: English
ISBN-10: 0930403347
ISBN-13: 978-0930403348
Product Dimensions: 1.2 x 6.5 x 9.8 inches
Shipping Weight: 2.3 pounds
Average Customer Review: 5.0 out of 5 stars See all reviews (1 customer review)
Best Sellers Rank: #1,241,159 in Books (See Top 100 in Books) #117 in Books > Engineering & Transportation > Engineering > Aerospace > Propulsion Technology #483 in Books > Engineering & Transportation > Engineering > Energy Production & Extraction > Fossil Fuels #567 in Books > Science & Math > Reference
This is a great book for learning about gas turbines and rocket engines. Discusses the aerothermodynamics behind the engines. Overall great book!
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