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- W1498532400 abstract "This chapter deals with aircraft performance, that is, the capability of aircraft to execute certain maneuvers and to meet mission requirements. Aircraft performance is based on the study of the forces acting on an aircraft and the effects that these forces have on its flight path. The resulting motions are grouped into four main classes: (i) accelerated curved symmetric flight; (ii) steady straight symmetric flight; (iii) accelerated straight symmetric flight; and (iv) non-symmetric flight. The basic forces are weight, thrust, and aerodynamic force (lift and drag). Additionally, in curved flight a centrifugal force appears. Presented are a few of the most important key performance measures of fixed-wing aircraft together with approximate equations that have been used in aeronautics to assess such performance in the early design stage of an aircraft. Range and endurance expressions are derived and attention is given to the weight breakdown and payload-range relationship for transport aircraft.Keywords:flight-path-related performance;fixed-wing aircraft;mission profile;symmetric flight;straight flight;turning flight;takeoff;climb;range and endurance;descent;landing;weight breakdown;payload-range diagram" @default.
- W1498532400 created "2016-06-24" @default.
- W1498532400 creator A5049008139 @default.
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- W1498532400 date "2010-12-15" @default.
- W1498532400 modified "2023-09-26" @default.
- W1498532400 title "Fixed-Wing Aircraft Performance" @default.
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- W1498532400 doi "https://doi.org/10.1002/9780470686652.eae376" @default.
- W1498532400 hasPublicationYear "2010" @default.
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