ELEMENTS OF PROPULSION GAS TURBINES AND ROCKETS MATTINGLY PDF

Elements of Propulsion : Gas Turbines and Rockets. Jack D. 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.

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About the Book Elements of Propulsion: Gas Turbines and Rockets, Second Edition provides a complete introduction to gas turbine and rocket propulsion for aerospace and mechanical engineers. Textbook coverage has been revised and expanded, including a new chapter on compressible flow. Design concepts are introduced early and integrated throughout. Written with extensive student input, the book builds upon definitions and gradually develops the thermodynamics, gas dynamics, rocket engine analysis, and gas turbine engine principles.

JACK D. After serving the majority of his career teaching at the Air Force Academy and Air Force Institute of Technology he retired from active duty in and joined the faculty of Seattle University, retiring in as professor emeritus in Mechanical Engineering.

He has since focused on writing, teaching short courses, and consulting. Air Force in after 32 years of active-duty service. Skip to main content. Description About the Book Elements of Propulsion: Gas Turbines and Rockets, Second Edition provides a complete introduction to gas turbine and rocket propulsion for aerospace and mechanical engineers.

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Elements of Propulsion : Gas Turbines and Rockets

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Description 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 worked examples and numerous homework problems so that concepts are applied after they are introduced.

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