I'm facing a difficulty: in SpaceClaim, I wrote a script to represent an airfoil and to deform its leading edge (to be able to optimize it later).
I also perform two calculations in this script (the area of the modified leading edge and its curvilinear length) that I would like to use in the Workbench as output parameters.
I can't find a way to do this. Can someone help me?
Thank you in advance,