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.

Supporting Material for Chapter 5. Supporting Material for Chapter 7. Supporting Material for Chapter 8. lnlets, Nozzles, and Combustion Systems. Supplemental JANNAF Tables Software. Software User Guides.

Book Information
ISBN 9781624103711
Author Jack D. Mattingly
Format Hardback
Page Count 976
Imprint American Institute of Aeronautics & Astronautics
Publisher American Institute of Aeronautics & Astronautics