Aerothermodynamics توربین گاز و موشک نیروی محرکه Aerothermodynamics of Gas turbine and Rocket propulsion
- نوع فایل : کتاب
- زبان : انگلیسی
- نویسنده : G. Oates
- ناشر : American Institute of Aeronautics and Astronautics
- چاپ و سال / کشور: 1997
- شابک / ISBN : 9781563472411, 1-56347-241-4
Description
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
