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Old Oct 09, 2012, 12:02 PM
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Joensuu, Finland
Joined Mar 2002
1,751 Posts
I see, thanks for posting that. Now, if the aileron and flap are deflected a different amount, a v-shaped gap opens up between them. That must generate a vortex there. Is there any data about how much drag this will create and is there any merit in trying to keep the gap minimized by having aileron and flap deflections equal?
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