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- W2321829846 abstract "A theoretical study is made of the performance capabilities of a lift concept that utilizes a spanwise vortex over the upper surface of the wing. The vortex is generated by a vertical flap near the leading edge of the wing and maintained by suction through orifices in endplates at the wingtip. The analysis approximates the three-dimensional flow field with a two-dimensional configuration that is mapped by conformal transformation into the flow about a circle. Theoretical solutions for a range of flap and orifice configurations predict that section lift coefficients up to around 10 can be achieved. It is concluded that such a lift concept is applicable to STOL aircraft if the vortex can be adequately stabilized and if the endplate suction can be generated efficiently." @default.
- W2321829846 created "2016-06-24" @default.
- W2321829846 creator A5074781884 @default.
- W2321829846 date "1977-06-27" @default.
- W2321829846 modified "2023-10-16" @default.
- W2321829846 title "Lift enhancement by an externally trapped vortex" @default.
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- W2321829846 doi "https://doi.org/10.2514/6.1977-672" @default.
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