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- W19387453 abstract "Report presenting an investigation to evaluate the effects of nacelles and extended split flaps on the longitudinal characteristics of a wing-fuselage-tail combination of a type believed to be suitable for long-range high-speed airplanes. Wind tunnel tests to study the effects of the nacelles and flaps were conducted at a range of Mach and Reynolds numbers. Results regarding the effects of the nacelles with the tail off, effects of tail height, effects of nacelles with the tail on, and effects of flaps are provided." @default.
- W19387453 created "2016-06-24" @default.
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- W19387453 date "1953-06-05" @default.
- W19387453 modified "2023-09-27" @default.
- W19387453 title "The Effects of Nacelles and of Extended Split Flaps on the Longitudinal Characteristics of a Wing-fuselage-tail Combination Having a Wing with 40 Degrees of Sweepback and an Aspect Ratio of 10" @default.
- W19387453 hasPublicationYear "1953" @default.
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