Coriolis effect and the attachment of the leading edge vortex
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Publication:5364734
DOI10.1017/jfm.2017.222zbMath1383.76580OpenAlexW2611217757MaRDI QIDQ5364734
Publication date: 28 September 2017
Published in: Journal of Fluid Mechanics (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1017/jfm.2017.222
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Dual-stage radial–tangential vortex tilting reverses radial vorticity and contributes to leading-edge vortex stability on revolving wings ⋮ On the formation of three-dimensional separated flows over wings under tip effects ⋮ A theory on leading-edge vortex stabilization by spanwise flow ⋮ On the maintenance of an attached leading-edge vortex via model bird alula ⋮ Laminar separated flows over finite-aspect-ratio swept wings ⋮ Uncoupling the effects of aspect ratio, Reynolds number and Rossby number on a rotating insect-wing planform ⋮ Evolutionary shape optimisation enhances the lift coefficient of rotating wing geometries ⋮ An investigation of kinematic parameters and stroke function on stroke reversal for three-dimensional vortex structures around a flapping insect wing ⋮ How dorsal fin sharpness affects swimming speed and economy ⋮ The role of rotary motion on vortices in reverse flow
Cites Work
- Computational Methods for Fluid Dynamics
- Three-dimensional effects in hovering flapping flight
- Numerical study of the turbulent flow past an airfoil with trailing edge separation
- Three-dimensional flows around low-aspect-ratio flat-plate wings at low Reynolds numbers
- On the identification of a vortex
- Role of the tip vortex in the force generation of low-aspect-ratio normal flat plates
- Reynolds number and aspect ratio effects on the leading-edge vortex for rotating insect wing planforms
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