Download - Vortaflow technology description
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![Page 1: Vortaflow technology description](https://reader036.vdocuments.net/reader036/viewer/2022082702/55626c45d8b42a14048b55e3/html5/thumbnails/1.jpg)
Flow reattachment – improved aerodynamic downforce
![Page 2: Vortaflow technology description](https://reader036.vdocuments.net/reader036/viewer/2022082702/55626c45d8b42a14048b55e3/html5/thumbnails/2.jpg)
α ≈ 0
CL ≈ y
Normal angled wing
![Page 3: Vortaflow technology description](https://reader036.vdocuments.net/reader036/viewer/2022082702/55626c45d8b42a14048b55e3/html5/thumbnails/3.jpg)
α ≈ x
CL ≈ 2 y
Increased angle of attack
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α ≈ 2 x
CL ≈ 0,5 y
Separated airfoil
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α ≈ 2 x
CL ≈ 3 y
Increased CL with Vortaflow
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α ≈ 0 CL ≈ yα ≈ x CL ≈ 2 y
α ≈ 2 x CL ≈ 0,5 y
α ≈ 2 x CL ≈ 3 y
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Current technology With Vortaflow
Reynolds number ≈ 2 · 106
![Page 8: Vortaflow technology description](https://reader036.vdocuments.net/reader036/viewer/2022082702/55626c45d8b42a14048b55e3/html5/thumbnails/8.jpg)
Current technology With Vortaflow
Reynolds number ≈ 2 · 106
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Tests on a Porsche 996 GT3 RS
Result: 5% increase in
cornering speed
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Design progress:
Equations
Experiments
Experience