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- W2094858049 abstract "The energy and economic benefits of low-speed aerodynamic system technology applied to a modern 200-passenger, 2000-nmi range, twin engine jet transport are reviewed. Results of a new method to design flap systems at flight Reynolds number are summarized. The study contains the airplane high lift configuration drag characteristics and design selection charts showing the effect of flap technology on the airplane size and performance. The study areas include: wing and flap geometry, climb and descent speed schedules with partial flap deflection, flap system technology, and augmented stability. The results compare the improvements in payload from a hot, high elevation airport." @default.
- W2094858049 created "2016-06-24" @default.
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- W2094858049 date "1979-08-17" @default.
- W2094858049 modified "2023-09-25" @default.
- W2094858049 title "The size and performance effects of high lift system technology on a modern twin engine jet transport" @default.
- W2094858049 doi "https://doi.org/10.2514/6.1979-1795" @default.
- W2094858049 hasPublicationYear "1979" @default.
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