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/Aerothermodynamics of Gas Turbine Rocket Propulsion [With *]
Aerothermodynamics of Gas Turbine Rocket Propulsion [With *]

Aerothermodynamics of Gas Turbine Rocket Propulsion [With *] - Hardcover

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Availability:In StockContributor:Gordon C. Oates, G. Oates, American Institute of Aeronautics and AsSeries:Dias y Dias de PoesiaPublish date:1997-01-01Pages:456
Language:EnglishPublisher:AIAA (American Institute of Aeronautics & AstISBN-13:9781563472411ISBN-10:1563472414UPC:9781563472411Book Category:Technology & Engineering, Science, TransportationBook Subcategory:Aeronautics & Astronautics, Mechanics, AviationBook Topic:ThermodynamicsSize:9.22 x 6.30 x 1.37 inchesWeight:1.8827Product ID:SCAFN5KZ9V
This seminal book on gas turbine technology has been a bestseller since it was first published. 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 flow 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, He and PC given, isentropic expansion).
Language:EnglishPublisher:AIAA (American Institute of Aeronautics & AstISBN-13:9781563472411ISBN-10:1563472414UPC:9781563472411Book Category:Technology & Engineering, Science, TransportationBook Subcategory:Aeronautics & Astronautics, Mechanics, AviationBook Topic:ThermodynamicsSize:9.22 x 6.30 x 1.37 inchesWeight:1.8827Product ID:SCAFN5KZ9V
Publisher: AIAA (American Institute of Aeronautics & Ast

Edition

3rd Edition

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