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Affecting Wingtip Vortex Using Wing Surface Contours

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Figure

Figure 1. Front and Top View of CGS Hawk light-weight sport aircraft. It is hypothesized that the ribsact as ridges which disrupt the spanwise flow over the wings thereby increasing the efficiency.
Figure 3. Flow visualization of Eppler 398 a.) bumpy b.) smooth wing at Re = 25000, = 4 degrees [5]
Figure 5. SolidWorks model of an AR 4 NACA 0012 wing with 12 surface contoured segments
Figure 7. University of Dayton Low-Speed Wind Tunnel (UD-LSWT) in the open-jet configuration.
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