Advanced Aircraft Flight Performance - Antonio Filippone

Advanced Aircraft Flight Performance

Buch | Hardcover
664 Seiten
2012
Cambridge University Press (Verlag)
978-1-107-02400-7 (ISBN)
93,50 inkl. MwSt
Covering aircraft flight performance, this book focuses on commercial aircraft, with some examples of military aircraft. A multidisciplinary engineering analysis is supported by flight simulation, with software validation at several levels. Environmental performance is discussed at four levels: aircraft noise, contrail effects, landing and take-off emissions and carbon dioxide emissions.
This book discusses aircraft flight performance, focusing on commercial aircraft but also considering examples of high-performance military aircraft. The framework is a multidisciplinary engineering analysis, fully supported by flight simulation, with software validation at several levels. The book covers topics such as geometrical configurations, configuration aerodynamics and determination of aerodynamic derivatives, weight engineering, propulsion systems (gas turbine engines and propellers), aircraft trim, flight envelopes, mission analysis, trajectory optimisation, aircraft noise, noise trajectories and analysis of environmental performance. A unique feature of this book is the discussion and analysis of the environmental performance of the aircraft, focusing on topics such as aircraft noise and carbon dioxide emissions.

Dr Antonio Filippone's expertise is in the fields of computational and experimental aerodynamics, flight mechanics, energy conversion systems, propulsion systems, rotating machines (helicopter rotors, propellers, wind turbines), systems engineering, and design and optimisation. He has published more than eighty technical papers, ten book chapters and two books, including Flight Performance of Fixed and Rotary Wing Aircraft (2006). Dr Filippone has been at the University of Manchester since 2000. Prior to this appointment, he was a research scientist at the Technical University of Denmark where he also received his PhD degree in 1996 for his research on rotor blade aerodynamics. He started his career at Risø National Laboratories, in Denmark, working on the aerodynamics of wind turbines.

1. Prolegomena; 2. Aircraft models; 3. Weight and balance performance; 4. Aerodynamic performance; 5. Engine performance; 6. Propeller performance; 7. Aeroplane trim; 8. Flight envelopes; 9. Take-off and field performance; 10. Climb performance; 11. Descent and landing performance; 12. Cruise performance; 13. Manoeuvre performance; 14. Thermo-structural performance; 15. Mission analysis; 16. Aircraft noise: noise sources; 17. Aircraft noise: propagation; 18. Aircraft noise: flight trajectories; 19. Environmental performance; 20. Epilogue.

Erscheint lt. Verlag 17.12.2012
Reihe/Serie Cambridge Aerospace Series
Zusatzinfo 69 Tables, unspecified; 5 Halftones, unspecified; 332 Line drawings, unspecified
Verlagsort Cambridge
Sprache englisch
Maße 180 x 257 mm
Gewicht 1300 g
Themenwelt Natur / Technik Fahrzeuge / Flugzeuge / Schiffe Luftfahrt / Raumfahrt
Mathematik / Informatik Mathematik Angewandte Mathematik
Mathematik / Informatik Mathematik Finanz- / Wirtschaftsmathematik
Technik Fahrzeugbau / Schiffbau
Technik Luft- / Raumfahrttechnik
ISBN-10 1-107-02400-5 / 1107024005
ISBN-13 978-1-107-02400-7 / 9781107024007
Zustand Neuware
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