Thank you for your quick reply !
I understood that non-zero displacements may be specified for restrained dof's and non-zero forces for unrestrained dof's, and I understood what you said.
As I could not manage to apply these (simple) boundary conditions(*), I tried to use the AXIS SYMMetric. I changed the geometry to respect the r-z coordinates with z as the axis. It looks more coherent, but I’m still not sure how I can apply the load.
SOLUTION 1 :
Using CSUR to apply a pressure, like in the plastic example
=>I get an error. I check on the forum but this is still unclear to me.
-->Contact check
*ERROR* Residual norm is NaN or Inf
SOLUTION 2 :
Using a Pressure MATErial tied with the ball, with TIE REGIon or TIE MATErial
=>It does not converge during CONTact CHECk. As no full convergence is obtained for the Newton solution strategy, I tried the manual option
LOOP augment a-iters
AUGMent
LOOP newton n-iters
CONTact CHECk
TANGent,,1
NEXT newton
NEXT augment
I got less warnings but a wrong solution.
SOLUTION 3 :
Using EFORce with the force in Newton applied on each node knowing that the factor 2pi is not included in any applied
loads.
=>In this case I noticed that the nodal force was not constant on each node, specially on the node located on the axis symmetric. I suppose this is due to a superposition of loads created by the symetry. (*)
I can't find where I'm wrong, any help would be appreciated.
(And thank you, TPLOt will do the trick. I need these reference points to interpolate the stress field, as I'll add inclusions distributed in the thrust washer according to a random space distribution.)
(*) I got "Internal server error" if I upload the picture