Flight Performance of Fixed and Rotary Wing AircraftElsevier, 10 Μαΐ 2006 - 600 σελίδες Calculation and optimisation of flight performance is required to design or select new aircraft, efficiently operate existing aircraft, and upgrade aircraft. It provides critical data for aircraft certification, accident investigation, fleet management, flight regulations and safety. This book presents an unrivalled range of advanced flight performance models for both transport and military aircraft, including the unconventional ends of the envelopes. Topics covered include the numerical solution of supersonic acceleration, transient roll, optimal climb of propeller aircraft, propeller performance, long-range flight with en-route stop, fuel planning, zero-gravity flight in the atmosphere, VSTOL operations, ski jump from aircraft carrier, optimal flight paths at subsonic and supersonic speed, range-payload analysis of fixed- and rotary wing aircraft, performance of tandem helicopters, lower-bound noise estimation, sonic boom, and more.This book will be a valuable text for undergraduate and post-graduate level students of aerospace engineering. It will also be an essential reference and resource for practicing aircraft engineers, aircraft operations managers and organizations handling air traffic control, flight and flying regulations, standards, safety, environment, and the complex financial aspects of flying aircraft.
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Περιεχόμενα
Part II RotaryWing Aircraft Performance | 299 |
Part III VSTOL and Noise Performance | 433 |
Appendix A Aircraft models | 479 |
Appendix B Noise data | 507 |
Appendix C Selected simulation programs | 509 |
531 | |
553 | |
Άλλες εκδόσεις - Προβολή όλων
Flight Performance of Fixed and Rotary Wing Aircraft Antonio Filippone Δεν υπάρχει διαθέσιμη προεπισκόπηση - 2006 |
Flight Performance of Fixed and Rotary Wing Aircraft Antonio Filippone Δεν υπάρχει διαθέσιμη προεπισκόπηση - 2006 |
Flight Performance of Fixed and Rotary Wing Aircraft Antonio Filippone Δεν υπάρχει διαθέσιμη προεπισκόπηση - 2006 |
Συχνά εμφανιζόμενοι όροι και φράσεις
acceleration advance ratio aerodynamic after-burning aileron air speed aircraft model aircraft weight airfoil airframe airplane analysis angle of attack atmospheric autorotation blade Boeing Calculate climb rate configuration constant decreases descent disk drag equation effects energy engine power engine thrust equation estimated fenestron fixed-wing aircraft flight altitude flight conditions flight path forward flight fuel consumption fuel flow glide ratio gross weight ground GTOW helicopter helicopter rotor hover increases induced power induced velocity ISA conditions jet aircraft km/h landing level flight lift coefficient Mach number main rotor maneuver mass maximum method minimum momentum theory MTOW NACA noise operation optimal parameters payload pitch power required pressure problem profile power propeller propulsion radius range reference rotational speed rotor power runway sea level shown in Figure solution subsonic supersonic tail rotor temperature transonic V/STOL vertical wing