Wingtip vortices in a wingsuit.

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The discussion centers on the impact of wingtip vortices created by a wingsuit flyer on the aerodynamics of the leg-wing. It suggests that the vortices generated by the arm-wings may not significantly affect drag due to the small weight of the human body compared to the overall drag of the wingsuit. The arm-wings are typically spread wider than the leg-wings, which may keep the legs below the path of the vortices. The conversation also questions whether these vortices could increase or decrease drag on the leg-wing, with a consensus that they likely harm laminar flow and do not provide aerodynamic benefits. Ultimately, the difference in drag experienced by the leg-wing in still air versus vortice-affected air remains uncertain.
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If you are not familiar with what a wingsuit is- you should google it.
Now...
Let's assume we have ourselves a wingsuit flyer in flight (or rather glide). Let's assume the arm-wings produce vortices on the wingtips and that these vortices hit the wingtips of the leg-wing ( which are where the feet are ).
Does that increase or reduce drag on the leg-wing?
What do you think is the effect of the arm-wing downwash on the leg wing?
(glide ratios for wingsuits are about 3:1 nowadays)


Cheers
 
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I doubt wingtip vortices from such a small falling weight as a human are a significant drag force, compared to the overall drag of the "aircraft". In addition, the arms are usually spread wider than the feet. Finally, it seems to me that for a glide ratio of 3:1, the legs would constantly remain below the vortices' path.
 
As for the vortice-path and glide ratio- the vortice may hit the feet. The angle of attack varies, and the hands may be positioned in such a way that the vortice lines go 'through' the feet (leg-wing wingtips).
IF they do, even if thay are small, do they increase drag on the legs or do they decrease it?
 
I can't see how it can help, and my best argument is that I can't think of any aircraft that has any parts of itself flying into its own vortices. In general, they harm laminar flow. I think you would need a very special and particular geometry for vortices to be somehow helpful to flight, and I'm not aware of any such geometry at the moment.
 
Let me then put it this way. The leg-wing of the wingsuit (and let's concentrate on the wingtips / feet) gliding through :
1) still air
2) "vortice-affected" air
What will be the difference in aerodynamic DRAG that the leg-wing experiences in 1) and 2) ?
 
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