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- W78833132 abstract "Gross size and weight characteristics estimated in previous chapters are used to select engines for the proposed aircraft. An introduction to landing requirements is presented after which landing wing loading and the effects of landing field length constraints are determined. Similar attention is paid to takeoff wing loading limitations in terms of takeoff distance. Constraints posed by the need for economical cruise are factored into the design process. These factors influencing the design are then combined into a single engine selection design chart. High-bypass turbofan engines and turboprop engines are discussed. Methods for determining net thrust in takeoff and in cruise are considered along with the effects of specific fuel consumption in cruise. A similar approach for the evaluation of turboprops in terms of takeoff distance and cruise capabilities is described. Safety considerations in one-engine-out operation and their application to requirements for a balanced field length are discussed." @default.
- W78833132 created "2016-06-24" @default.
- W78833132 creator A5074583556 @default.
- W78833132 date "2014-01-01" @default.
- W78833132 modified "2023-10-16" @default.
- W78833132 title "Engine Selection" @default.
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- W78833132 doi "https://doi.org/10.1016/b978-0-12-419953-8.00004-8" @default.
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