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Originally Posted by Crumpp
It does move to the left when TE flaps deploy.
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Then why do you say the opposite, first?
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In this case though you claimed that the top polars were different designs of TE flaps deployed and their effect. They were different designs of radiator flaps as I stated...
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The Messerschmitt engineers referred to them as trailing edge flaps, but since the radiator flap was part of the trailing edge flap, I don't even understand what point you're trying to make now?
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Therefore, the curve in question on the bottom would be shifted to the right if that was the case.
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The curve on the bottom would shift to the right if wing camber increased? It wouldn't. In case I misread you, can you please post a little bit more coherent (leaving out the "u suck I rule" stuff would help)?
You could still explain how you see that the slats deploy within the 2.5° between 8 and 11.5° AoA as you said. From where I am standing, it is not on the chart.