CAE (I) Chapter 16. Convergence of Nonlinear Analysis

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Page 49

Example: Hyperelastic Planar Seal

  1. Construct the FE model

  2. Enter solution and impose 0.85ˇ¨ of deflection in the ˇVY direction at the pilot node (n_load).

  3. Activate nonlinear geometry (NLGEOM).

  4. Set ˇ§timeˇ¨ equal to the absolute value of the imposed displacement.

  5. Set the number of substeps for automatic time stepping. Try NSUBST, 25, 200, 20. (If you have time you can experiment with the number of substeps to see how this affects the convergence behavior of the problem.)

  6. Monitor the reaction force at the pilot node (n_load) as variable 3 in the monitor file.

  7. Set the output controls to write every substep to the .rst file (OUTRES).

  8. Solve the problem.

  9. Review the results in the general postprocessor. Plot the deformed shape, stress results, and contact pressures.

  10. Plot the force deflection curve in the time history postprocessor.

  11. Review the output file and the monitor file. At what point in the solution does the program have difficulty converging? Why?

  12. If you have time rerun the analysis including friction. (Set MU = 0.2 for material 1.) Note the convergence behavior. Does including friction take more or less iterations? Plot the force deflection curve. What happens to the reaction force required to compress the seal?