Phase 2: Determine the Superelement
Create a Set for the Strut and Boundary Elements
Create a Set for Boundary Nodes
Create ASET Constraints
Delete Residual Set Element
The reduced stiffness and mass matrix are generated for only those elements that are reduced out (superelement). Therefore, a new model needs to be created containing just the superelement part and the loads and boundary conditions applied directly to that part.
Define CMS Method Entry
The CMSMETH load collector triggers the creation of the reduced matrices.
Run the CMSMETH Global Case Control
Save the Model
Save as a new model.
- Click .
- For File name, enter airframe_section_SUPERELEMENT_CMS.hm.
- Click Save.