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What's the reason for the local flap extensions at the shockbody locations?

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This weekend I was on a Airbus A319, and I noticed that the flaps have small extensions at the location of the shockbodies (indicated in the picture with the red circles)

I was wondering what the reason is for these extensions?

My guess is that it could be to compensate for the lower local lift generation caused by the presence of the shock bodies, but I'm not sure. I'm also interested in knowing why they have different sizes at different locations.

enter image description here


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