Abstract
The objective of the present paper is improving the effectiveness of a winglet control surface at deflections greater than ≈5° through passive vortex generators (VG) placed on the control surface. Without deflection, the VGs are aligned with the flow direction and thus have almost no impact. The conceptual idea is that a control surface deflection changes the flow direction in such a way that the VGs become active and delay flow separation from the trailing edge. To decide on an appropriate initial Vortex Generator (VG) configuration the aerodynamic characteristics of the winglet are investigated first with Reynolds averaged Navier–Stokes (RANS) simulations. The functional principle of the concept is then demonstrated. A parametric study of different VG dimensions investigates the effectiveness for a range of flow conditions and deflection angles.
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a callDisclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.
