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- W2066068130 abstract "Passive lift enhancement for flexible nonslender delta wings has been demonstrated as a potential method for the control of vortex-dominated wing flows. Physical mechanisms of lift enhancement and the effect of important variables are discussed. Lift enhancement for flexible wings with low/moderate sweep is a very complex phenomenon, involving self-induced antisymmetric vibrations of leading edges, spanwise camber effect due to the large time-averaged deflection, shear layer instabilities, reattachment, increased mean vorticity flux and circulation, re-formation of the leading edge vortices, possible enhancement of streamwise pressure gradient, and the effects of frequency and edge velocity." @default.
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- W2066068130 date "2005-01-10" @default.
- W2066068130 modified "2023-09-23" @default.
- W2066068130 title "Physical Mechanisms of Lift Enhancement for Flexible Delta Wings" @default.
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- W2066068130 doi "https://doi.org/10.2514/6.2005-867" @default.
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