Theory of Aerospace Propulsion

2 ed
ISBN: 978-0-12-809326-9
Verlag: Elsevier - Health Sciences Division

Buch, Englisch, 848 Seiten, Format (B × H): 241 mm x 194 mm, Gewicht: 1610 g

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.

Zielgruppe

Undergraduate and graduate level students in aerospace or mechanical engineering studying aerospace propulsion or turbomachinery. Aerospace or mechanical engineers working in gas turbines, turbomachinery, aircraft propulsion and rocket propulsion.

Autoren/Hrsg.

Sforza, Pasquale M.

Fachgebiete

• Technische Wissenschaften Maschinenbau | Werkstoffkunde Maschinenbau Triebwerkstechnik, Energieübertragung
• Technische Wissenschaften Maschinenbau | Werkstoffkunde Technische Mechanik | Werkstoffkunde Strömungslehre
• Technische Wissenschaften Verkehrstechnik | Transportgewerbe Luft- und Raumfahrttechnik, Luftverkehr
• Naturwissenschaften Physik Mechanik Kontinuumsmechanik, Strömungslehre

Inhaltsverzeichnis

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

Über Autor(innen)

Sforza, Pasquale M.
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)