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Variations in the wake structure of non-elliptical lift distributions near wingtip

Schreyer, Grace
Gunasekaran, Sidaard
Pabon, Julian A.
Cai, Jielong
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2025-01-03
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Conference paper
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Keywords
Zero lift drag coefficient,Vortex structure,Aerodynamic performance,Particle image velocimetry,Low speed wind tunnel,Wing configurations,Numerical simulation,Shear layers,Rectangular wing,Aspect ratio
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Grace A. Schreyer, Sidaard Gunasekaran, Julian A. Pabon and Jielong Cai. "Variations in the Wake Structure of Non-Elliptical Lift Distributions Near Wingtip," AIAA 2025-0253. AIAA SCITECH 2025 Forum. January 2025.
Abstract
Non-elliptical lift distributions, particularly bell-shaped distributions with extended spans, have shown potential to disrupt conventional tip vortex roll-up, even eliminating trailing vortices in the near wake. This study investigates the aerodynamic performance and near-wake characteristics of four wing configurations: a baseline untwisted wing, an elliptically loaded wing, and two nonelliptical lift distributions. Force-based experiments and streamwise Particle Image Velocimetry (PIV) were conducted in the University of Dayton Low-Speed Wind Tunnel (UD-LSWT), with results compared to numerical simulations using FlightStream®. The findings reveal that, at moderate CL, wings with non-elliptical lift distributions exhibit a near-planar wake with no discernible trailing vortex signature, while the elliptically loaded wing demonstrates clear trailing vortex roll-up. Additionally, the non-elliptical configurations displayed reduced downwash and thinner wake structures compared to other configurations. These results underscore the distinct wake characteristics of non-elliptical lift distributions, marking a significant deviation from traditional trailing vortex behavior.
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This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) license (https://creativecommons.org/licenses/by/4.0/).
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American Institute of Aeronautics and Astronautics Inc, AIAA
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AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2025
6 January 2025 through 10 January 2025
Orlando
325579
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