Thanks DaveW – that’s a very neat description.
The FIA testing point is roughly in line with the pylons. So to get the correct test results, the elastic shear centre of the section will be at that point so the wing appears to be stiff. Meanwhile the centre of aero pressure is much further back because that’s where the wing cascade is located. I suspect RB are exploiting the resulting eccentric forces to cause the wing to deflect.
The issue of divergence is interesting. I guess this could lead to a positive feedback whereby the ground effect forces pull the wing further down than it would if it were operating in free air?