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Separated flows over swept wings across transitional Reynolds numbers
We explore the effect of wing sweep on the interaction between leading-edge separation and tip vortex for a finite wing with sweep angles $Λ=0^\circ$ to $45^\circ$, semi-aspect-ratio $sAR=2$, angle of attack $14^\circ$, and chord-based Reynolds numbers $Re=600$, $1000$, $2500$, $5000$, and $10000$.
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