Interplay of the leading-edge vortex and the tip vortex of a low-aspect-ratio thin wing

Lei Dong, Kwing So Choi*, Xuerui Mao

*Corresponding author for this work

Research output: Contribution to journalArticlepeer-review

12 Citations (Scopus)

Abstract

Abstract: Three-dimensional vortical structures and their interaction over a low-aspect-ratio thin wing have been studied via particle image velocimetry at the chord Reynolds number of 10 5. The maximum lift of this thin wing is found at an angle of attack of 42 . The flow separates at the leading-edge and reattaches to the wing surface, forming a strong leading-edge vortex which plays an important role on the total lift. The results show that the induced velocity of the tip vortex increases with the angle of attack, which helps reattach the separated flow and maintains the leading-edge vortex. Turbulent mixing indicated by the high Reynolds stress can be observed near the leading-edge due to an intense interaction between the leading-edge vortex and the tip vortex; however, the reattachment point of the leading-edge vortex moves upstream closer to the wing tip. Graphic abstract: [Figure not available: see fulltext.].

Original languageEnglish
Article number200
JournalExperiments in Fluids
Volume61
Issue number9
DOIs
Publication statusPublished - 1 Sept 2020
Externally publishedYes

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Dong, L., Choi, K. S., & Mao, X. (2020). Interplay of the leading-edge vortex and the tip vortex of a low-aspect-ratio thin wing. Experiments in Fluids, 61(9), Article 200. https://doi.org/10.1007/s00348-020-03023-4