[CATIA] Airframe Composites Designer

Functional Value

Laminates in the Composites Parameters can now be defined with a targeted thickness and corresponding ratio per orientation. The targeted thickness is exposed as a knowledge parameter.

I
What's new for Composites in R2022x FD02 video

I
Define laminates based on the conceptual reference thickness value by assigning ratios for each orientation per material.

I
Automatic computation of the number of layers based on reference thickness along with visual indication of the thickness achieved.

I
The thickness law, number of layers, and actual thickness all update automatically when the target thickness parameter is changed, making Composites conceptual design exploration quick and easy.