Hello,

I need to create a constant thickness of 0.42mm at the back of an airfoil (the thickness at the root and tip of the airfoil needs to be the same, 0.4-0.5mm, in this example 0.42mm as defined by the root profile). "create a constant thickness" means cut away the part that's thinner

The remaining of the airfoil needs to maintain the original cross section shape (it's scaled).

Can this be done?

S.