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- W814296479 abstract "Characteristics of trailing vortices generated by a rectangular fixed wing with the NACA23012 airfoil section have been investigated with a 2-dimensional LDV system. Curved slots were imbedded near the rectangular tip to blow a slight amount of the main stream into the tip face and to modify tip vortices. Tangential and axial velocity components of tip vortices, circulations and momentum deficits were measured at vertical planes to the vortex trail for both the plain and the slotted wings, respectively. Lift distributions over both wings were also investigated by the use of the bound dirculations measured at five different locations for each span. It was found that the slotted wing develops a fairing effect at the tip and lessens the vortex strengths without serious defects for the lift losses even though the slight momentum deficit was perceived for this selected model. It was, therefore, confirmed that the slotted wing can be used for a device to improve the aerodynamic performance by the tip vortex modification." @default.
- W814296479 created "2016-06-24" @default.
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- W814296479 date "1999-01-01" @default.
- W814296479 modified "2023-10-06" @default.
- W814296479 title "Modification of Tip Vortex by Spanwise Slots" @default.
- W814296479 hasPublicationYear "1999" @default.
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