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Defining Ansys Superelement SUB File Manually

Photo by  James Owen  on  Unsplash A surprisingly popular blog-post written here is Exporting Stiffness Matrix from Ansys . A sensible follow up question is what can one do with the exported stiffness matrix? In a recent Xansys Forum post, a question was raised on how we can edit the stiffness matrix of a superelement and use it for our model.  An approach presented below is to first create a superelement that has the same number of DOF and nodal location that will serve as a template. An APDL script can then be written to edit the stiffness matrix entries as desired before exporting to a new superelement *.SUB file for use in future models. The self-contained script below demonstrates this.  /prep7 et ,1, 185 mp , ex, 1, 200e3 mp , prxy, 1, 0.33 w = 0.1 ! single element (note nodal locations) n , 1, w, -w, -w n , 2, w, w, -w n , 3, -w, w, -w n , 4, -w, -w, -w n , 5, w, -w, w n , 6, w, w, w n , 7, -w, w, w n , 8, -w, -w, w e , 1, 2, 3, 4, 5, 6, 7, 8 /solu antype , substr     ! analy

Non-linear Convergence

Saying a Prayer*

In the few tingling seconds between saving the project and hitting Solve on Ansys, I would mutter a prayer under my breath. There is always an indescribable brief sense of helplessness and hope. Non-linear problems are tough because... they are nonlinear! A small nudge can have disproportional effects. 

Learning how to solve non-linear problems takes patience and luck. Here are some resources which I found useful in my journey in learning the secret arts (in no particular order):
1. CAEAI: Best Practices (link) (backup_link)
2. Joseph Metrisin1: contact convergence debugging guidelines (link) (backup_link)
3. Rod Scholl: contact analysis guidelines (link) (backup_link)
4. Ansys: Could you give me tips and tricks for Non-linear simulations? (link)
5. John Higgins: Obtaining and Optimizing Structural Analysis Convergence (link)
6. PADT: Overcoming Convergence Difficulties (Part I & II)
7. Ansys: Snap Fit Analysis - Best Practice (link)
8. Charlie Wells: Xansys words-of-wisdom (link)

It is no doubt worth reading the lecture notes on Basic Structural Nonlinearities with ANSYS Mechanical 17.0 (link)

Some of the best tips I found useful: 
1. Align nodes between contact and target if possible in the sliding direction (link)
2. Save Newton-Raphson Residuals & Identify Element Violation before analysis starts (link)
3. Use MPC for bonded contacts if needed (link).
4. Set small initial time steps. Here is my default setting for difficult problems:

The first step would thus be 1/100= 0.01s with a minimum time step of 1/1000= 0.001s. Apply this to all "Current Step Number" of interest.

5. Have similar size mesh at contacts. If not, Contact has finer mesh while Target is coarser.
6. Slice and dice geometry such that the volumes adjacent to contacts can be Hexahedron elements. 
         - Starting with pretty mesh by the contacts reduces the distortion during the analysis. 
         - Hexahedron elements are less distorted when capturing curved geometries (e.g. holes). 
7. Drop Contact Normal Stiffness Factor (i.e. FKN) to 0.01. Watch out for excessive penetration.
8. Use Contact Tool to see if any contacts are open. Pinball radius may need tweaking. 
9. Switch model to Displacement driven instead of Force driven for better stability. 
10. Avoid over-constrained model whenever possible (e.g. symmetry and bonded contacts) 
11. Move the body to be just in contact so that it doesn't 'fly' a small distance before touching. 

What Next?
There are more complicated techniques when desperate like ramping up FKN using RMODIF gradually. Another is to swap out displacement driven to force driven mid-flight. Many more are described in the links above. Hopefully more exotic techniques aren't required. Otherwise, as Bon Jovi famously sang...
Woah, we're half way there 
Woah, livin' on a prayer 
Take my hand, we'll make it I swear 
Woah, livin' on a prayer

Good luck!

1Bow your head towards Canonsburg and pray to the Ansys gods before clicking solve - Joe


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