Hello.
I am trying to do a static analysis of a torque box using shell elements and I have the following issue.
I have modeled the Boeing 737 wing (torque box) in Autodesk Inventor using surfaces.
Then I transferred it in Ansys Workbench to start the FEA analysis.
However, I want the inner structure of the wing to be made using composite materials.
So, I opened an ACP module. In that module, I cannot hide some surfaces and here's where the problem is.
If I can't hide them, then I cannot select the ribs and apply an Oriented Selection Set.
I tried, also, making three different ACP modules and then assembling them in static structural (transferring shell data) however that results into an error.
I have attached my project file, without the ACP module.
Nils Wagner
Hello sir,
Thank you for an early reply.
However I am modeling in Ansys Workbench and Mechanical and not in Mechanical APDL.
I wrote input files and attached them here.
Marios Stylianou
Thank you for sharing your .cdb file. Please can also you provide the material properties of the composite?
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