Ben
My thought is to reduce the thickness and camber of the wing near the top. This will reduce the lift coefficient even when the apparent wind at the top has a higher angle of attack than the bottom of the wing experiences. A constraint would be not to increase the feathered drag markedly so there could be some fiddling with the edge radius to find the best result.
Rick
On 19/07/2011, at 12:07 PM, bjarthur123 wrote:
care to elaborate? do you have ideas on how to twist your wing, both to accommodate the wind shear as well as to feather just the top??
ben
> The twisting could be achieved through more subtle means than actual
> twist.
Rick Willoughby
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