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And airfoils are designed with great care to avoid turbulence and the inevitable increase in drag. Rick. |
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Edit: where are you in Lousiana? I lived in Baton Rouge for a couple of years, back around 2000 or so. |
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USA, ME, Ellsworth
Joined May 2008
13,873 Posts
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It is kind of quiet over here. All we wanted is to know a little bit about the KF airfoils as they compare to some of the old standards, right?
Today, on another thread about wind tunnel sensors, poster Odysis said the following: Quote:
I think Odysis hit the nail on the head when he said it is not trivial... Happy Holidays to all! Jack |
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That wind tunnel link is indeed interesting. It's a complex area.
I read recently that in the early days the English and the Americans both had State Of The Art tunnels. They were both confident that they were doing good science. After some time some the thought occurred that they should exchange some test models and see if their testing could be replicated. The results were so random that it was clear that both tunnels needed a serious re-think. However, that's a problem confined to testing that can be extrapolated to other cord sizes and Rn. For Comparative Testing where, say a KFm2 and a Clark Y were compared for lift and drag under the same conditions, meaningful information could be obtained. If the air speed and wing cord were both in the 'real world' range, no scale effects would complicate matters and Mr Renolds would be happy. It's still complicated though... |
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Joined Mar 2008
580 Posts
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This is not a new problem. |
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