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Antriebselemente: Gasturbinen und Raketen von Jack D Mattingly: gebraucht

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Artikelzustand
Gut: Buch, das gelesen wurde, sich aber in einem guten Zustand befindet. Der Einband weist nur sehr ...
Publication Date
2006-08-01
Pages
867
ISBN
9781563477799
Book Title
Elements of Propulsion : Gas Turbines and Rockets
Book Series
Aiaa Education Ser.
Publisher
American Institute of Aeronautics & Astronautics
Item Length
9.2 in
Publication Year
2006
Format
Hardcover
Language
English
Illustrator
Yes
Item Height
2 in
Author
Jack D. Mattingly
Genre
Transportation, Technology & Engineering
Topic
Aviation / General, Aeronautics & Astronautics
Item Weight
57.2 Oz
Item Width
6.3 in
Number of Pages
867 Pages

Über dieses Produkt

Product Identifiers

Publisher
American Institute of Aeronautics & Astronautics
ISBN-10
1563477793
ISBN-13
9781563477799
eBay Product ID (ePID)
63718531

Product Key Features

Book Title
Elements of Propulsion : Gas Turbines and Rockets
Number of Pages
867 Pages
Language
English
Topic
Aviation / General, Aeronautics & Astronautics
Publication Year
2006
Illustrator
Yes
Genre
Transportation, Technology & Engineering
Author
Jack D. Mattingly
Book Series
Aiaa Education Ser.
Format
Hardcover

Dimensions

Item Height
2 in
Item Weight
57.2 Oz
Item Length
9.2 in
Item Width
6.3 in

Additional Product Features

Intended Audience
Trade
LCCN
2006-017363
Dewey Edition
22
Dewey Decimal
629.134/353
Synopsis
This text provides a complete introduction to gas turbine and rocket propulsion for aerospace and mechanical engineers. Building on the very successful Elements of Gas Turbine Propulsion, textbook coverage has been expanded to include rocket propulsion and the material on gas dynamics has been dramatically improved. The text is divided into four parts: basic concepts and gas dynamics; analysis of rocket propulsion systems; parametric (design point) and performance (off-design) analysis of air breathing propulsion systems; and analysis and design of major gas turbine engine components (fans, compressors, turbines, inlets, nozzles, main burners, and afterburners). Design concepts are introduced early (aircraft and rocket performance in an introductory chapter) and integrated throughout. Written with extensive student input on the design of the book, the book builds upon definitions and gradually develops the thermodynamics, gas dynamics, rocket engine analysis, and gas turbine engine principles. The book contains over 100 worked examples and numerous homework problems so concepts are applied after they are introduced. examples. Eight computer programs accompany the text, which allow for rapid calculation of trends, what if questions, conceptual design, homework problems, and homework verification. The software runs in the Windows operating system on PC-compatible systems., This text provides a complete introduction to gas turbine and rocket propulsion for aerospace and mechanical engineers. Building on the very successful "Elements of Gas Turbine Propulsion," textbook coverage has been expanded to include rocket propulsion and the material on gas dynamics has been dramatically improved. The text is divided into four parts: basic concepts and gas dynamics; analysis of rocket propulsion systems; parametric (design point) and performance (off-design) analysis of air breathing propulsion systems; and analysis and design of major gas turbine engine components (fans, compressors, turbines, inlets, nozzles, main burners, and afterburners). Design concepts are introduced early (aircraft and rocket performance in an introductory chapter) and integrated throughout. Written with extensive student input on the design of the book, the book builds upon definitions and gradually develops the thermodynamics, gas dynamics, rocket engine analysis, and gas turbine engine principles. The book contains over 100 worked examples and numerous homework problems so concepts are applied after they are introduced. Over 600 illustrations and pictures show basic concepts, trends, and design examples. Eight computer programs accompany the text, which allow for rapid calculation of trends, lwhat ifn questions, conceptual design, homework problems, and homework verification. The software runs in the Windows operating system on PC-compatible systems., This text provides a complete introduction to gas turbine and rocket propulsion for aerospace and mechanical engineers. Building on the very successful Elements of Gas Turbine Propulsion, textbook coverage has been expanded to include rocket propulsion and the material on gas dynamics has been dramatically improved. The text is divided into four parts: basic concepts and gas dynamics: analysis of rocket propulsion systems; parametric (design point) and performance (off-design) analysis of air breathing propulsion systems; and analysis and design of major gas turbine engine components (fans, compressors, turbines, inlets, nozzles, main burners, and afterburners). Design concepts are introduced early (aircraft and rocket performance in an introductory chapter) and integrated throughout. Written with extensive student input on the design of the book, the book builds upon definitions and gradually develops the thermodynamics, gas dynamics, rocket engine analysis, and gas turbine engine principles. The book contains over 100 worked examples and numerous homework problems so concepts are applied after they are introduced. Over 600 illustrations and pictures show basic concepts, trends, and design examples. Eight computer programs accompany the text, which allow for rapid calculation of trends, "what if" questions, conceptual design, homework problems, and homework verification. The software runs in the Windows operating system on PC-compatible systems.
LC Classification Number
TL709.M388 2006

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