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
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
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)
"The authors of the book have managed to write book [sic] in a
manner where students can learn all the concepts from basic to
advance at one-stop location in form of this book. ...I strongly
recommend this textbook for aeronautical or aerospace students at
either undergraduate or postgraduate level. Aerospace
researchers/engineers will also find it useful as a handbook on all
basics." --The Aeronautical Journal
"The authors of the book have managed to write book in a manner
where students can learn all the concepts from basic to advance at
one-stop location in form of this book.
I strongly recommend this textbook for aeronautical or aerospace
students at either undergraduate or postgraduate level." --The
Aeronautical Journal
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