Abstract
AbstractVortex roll‐up processes of different generic wingtip shapes are investigated using the DLR TAU flow solver in combination with a Reynolds Stress Model. In contrast to a non‐rounded layout an elliptical rounding of the wingtip planform leads to multiple vortices at the wingtip and results in an axial velocity deficit in the vortex core further downstream. (© 2017 Wiley‐VCH Verlag GmbH & Co. KGaA, Weinheim)
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