montaviale
Guest
Good morning to all,
I write to ask you a problem:
My goal is to inspect a wing (a screenshot attached), I would need a script that locally computes the thickness of the wing at various points and increases the thickness of 10%. then on the exit edge where the thickness is very small about 1 tenth the thickness increase of both one cent, while at the maximum thickness point of the wing where the thickness is about 9 mm the thickness increase is 9 tenths. once calculated the increase in thickness in a set of points should reconstruct the surface of the back. Is it possible for you? I initially climbed into a dimension the back surface, considering fixed the points that are on the z=0 plane, that is the plan of division of the wing, at first approximation this method is correct but I would like to get a better result.
Thank you.
Faithful
I write to ask you a problem:
My goal is to inspect a wing (a screenshot attached), I would need a script that locally computes the thickness of the wing at various points and increases the thickness of 10%. then on the exit edge where the thickness is very small about 1 tenth the thickness increase of both one cent, while at the maximum thickness point of the wing where the thickness is about 9 mm the thickness increase is 9 tenths. once calculated the increase in thickness in a set of points should reconstruct the surface of the back. Is it possible for you? I initially climbed into a dimension the back surface, considering fixed the points that are on the z=0 plane, that is the plan of division of the wing, at first approximation this method is correct but I would like to get a better result.
Thank you.
Faithful
