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mat Redsell wrote:
Common knowlege about Glider wing designs says that a high taper ratio will lead to Wing tip stalls. However in our flights and research we have found that a straight or forward swept flying wing will not stall a wing tip despite the very narrow chord ( renolds numbers of 325,000) and lack of washout at the tip. I can attempt a stall in the Pioneer IId by bringing the stick slowly all the way back giving a CL of about 1.5 at 32 mph. We do have some separation at the root but there is no sudden wing tip stall despite no washout at the tips. The glider itself will not stall. The "modern" gliders don't have problems with tip stalls under the same straight ahead stalls, either. They might have some washout, but may instead use different airfoils at the root and tip. Winglets can also be used to prevent tip stalling, and many gliders now have swept back leading edges that probably reduce the tip stall likelihood. Taper ratio isn't a very useful predictor for this problem, and it is barely mentioned in Fundamentals of Sailplane Design. Turning stalls are the ones you need to study, because almost every glider can have a tip stall during a turn. In the gliders I also fly with tails, Grob 103 and 102 there is also a reluctance to not stall a wing tip but that is perhaps due to the washout at the tips. Does the wing tip stall suddenly in some of the high performance ships that may not have the amount of washout that the lower performing ships? What gliders if any do stall a wing tip easily? I don't think this is a problem in the "modern" high performance glider. The ones I've flown are generally quite benign in stalls, both straight ahead and turning. -- ----- change "netto" to "net" to email me directly Eric Greenwell Washington State USA |
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