Aerothermodynamics of Gas turbine and Rocket propulsion by G. Oates

Aerothermodynamics of Gas turbine and Rocket propulsion



Download Aerothermodynamics of Gas turbine and Rocket propulsion




Aerothermodynamics of Gas turbine and Rocket propulsion G. Oates
Language: English
Page: 459
Format: pdf
ISBN: 1563472414, 9781563472411
Publisher: AIAA (American Institute of Aeronautics & Ast

Includes software

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.

System Requirements:IBM PC 386/486/586/Pentium or compatible; 640 Kb RAM hard disk with 1.0 Mb of available disk space; EGA or better video capability

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