[Crumpp]

but I don't see how the trailing edge flaps suddenly became the issue.

Of course not....that would mean you spouted off without knowing the context or details, posting something to discredit whatever I said.

I'd think they move to the left,

It does move to the left when TE flaps deploy. A camber change shifts the lift curve reducing the AoA CLmax for the airfoil occurs.

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 in my first reply of too many to you.

Therefore, the curve in question on the bottom would be shifted to the right if that was the case. You started posting about the language used on the polar out of context and without the details.

JtD your focus is never on the topic at hand. It is only to discredit anything I say in any way that you can.

I have nothing further on this topic or any other topic for you. You can work whatever angle you dream up to claw at this conversation but I wish you good luck in your life.

The good thing is that by this way you hve an independent behavior for both slat that can result in asymmetric deployment

For the readers, asymmetric deployment is normal. As the slat works as required, it does not effect the flight of the aircraft at all compared to symmetrical deployment.

It only becomes a problem when if the slats experience a mechanical malfunction and one slat cannot meet the force required.