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#4
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At 04:12 07 January 2006, Bagmaker wrote:
OK, I can get the theory (OR can I?) with winglets to reduce wingti vortices. Surely the best direction for the tip is DOWN!, I understand this ma be difficult for actually making, especially with gliders an groundloops, aesthetics, etc, but can someone explain why they ar pointing up? Consider this.. The HIGH pressure area is UNDER the wing, we want to keep this fro migrating to the LOW pressure area ABOVE the wing. Our current wingti style will restrict the LOW pressure from bleeding sideways (and wh would it anyway) yet the majority (?) of our lift is generated from th HIGH pressure BELOW the wing. This high pressure is what we want to retain and utilise, yet it i still allowed to bleed out sideways. Sure the current shape of wingti will reduce the vortices caused by the two pressures meeting, and thu the drag, but it wont increase the lift available by retaining the HIG pressure UNDER the wing, where it is most useful. I also note the return of the 'plate' style winglet on lates jetliners, half above, half below the wingtip, instead of a larg winglet. Enlighten me, O knowledgable ones! It's not so much about blocking the flow since it's all going to mix once it gets aft of the wing anyway. The winglet actually reduces the vortex by creating circulation off the vortex itself - this is why a winglet is an airfoil and not just a plate. It flies in the local flow field at the tip and creates a lift vector that is inward and slightly forward (that's right forward lift - thrust!). I honestly don't know if pointing up versus down is for practical or aerodynamic reasons - I can't think of a reason why it would matter, you'd have to reverse the airfoil and reoptimize for the underside flow field. 9B |
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