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  3. Aerothermodynamics of Gas turbine and Rocket propulsion

Aerothermodynamics of Gas turbine and Rocket propulsion

Posted By: insetes
Date: 29 Mar 2021 10:53:45
Aerothermodynamics of Gas turbine and Rocket propulsion

Aerothermodynamics of Gas turbine and Rocket propulsion By G. Oates
1997 | 459 Pages | ISBN: 1563472414 | PDF | 6 MB


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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