Theory of Aerospace Propulsion / Edition 2

Theory of Aerospace Propulsion / Edition 2

by Pasquale M. Sforza
ISBN-10:
0128093269
ISBN-13:
9780128093269
Pub. Date:
08/26/2016
Publisher:
Elsevier Science
ISBN-10:
0128093269
ISBN-13:
9780128093269
Pub. Date:
08/26/2016
Publisher:
Elsevier Science
Theory of Aerospace Propulsion / Edition 2

Theory of Aerospace Propulsion / Edition 2

by Pasquale M. Sforza
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Overview

Theory of Aerospace Propulsion, Second Edition, teaches engineering students how to utilize the fundamental principles of fluid mechanics and thermodynamics to analyze aircraft engines, understand the common gas turbine aircraft propulsion systems, be able to determine the applicability of each, perform system studies of aircraft engine systems for specified flight conditions and preliminary aerothermal design of turbomachinery components, and conceive, analyze, and optimize competing preliminary designs for conventional and unconventional missions. This updated edition has been fully revised, with new content, new examples and problems, and improved illustrations to better facilitate learning of key concepts.


Product Details

ISBN-13: 9780128093269
Publisher: Elsevier Science
Publication date: 08/26/2016
Series: Aerospace Engineering
Edition description: Reprint
Pages: 848
Sales rank: 952,069
Product dimensions: 7.50(w) x 9.25(h) x (d)

About the Author

Pasquale Sforza received his PhD from the Polytechnic Institute of Brooklyn in 1965. He has taught courses related to commercial airplane design at the Polytechnic Institute of Brooklyn and the University of Florida. His research interests include propulsion, gas dynamics, and air and space vehicle design. Dr. Sforza has also acted as Co-Editor of the Journal of Directed Energy and Book Review Editor for the AIAA Journal. His previous books include Theory of Aerospace Propulsion (Butterworth-Heinemann, 2011) and Commercial Airplane Design Principles, (Butterworth-Heinemann, 2014)

Table of Contents

1. Propulsion Principles and Engine Classification2. Quasi-One-Dimensional Flow Equations3. Idealized Cycle Analysis of Jet Propulsion Engines4. Combustion Chambers for Airbreathing Engines5. Nozzles for Airbreathing Engines6. Inlets for Airbreathing Engines7. Turbomachinery8. Blade Element Theory for Axial Flow Turbomachines9. Airbreathing Engine Performance and Component Integration10. Propellers11. Liquid Propellant Rocket Motors12. Solid Propellant Rocket Motors13. Space Propulsion

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From the Publisher

Including new content, new examples and problems, and improved illustrations, this quantitative treatment of aerospace propulsion systems supports the analysis, integration, and design of components and systems for a wide range of conventional flight and unconventional missions

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