[DrAurora]

Hello comrades,

I would like to conduct stress analysis for backward curved axial fan (in the end).
For this and as a first step, I start testing a simple case by utilizing stress analysis/platehole.
The attaced image is for a test case.
Quarter-of-Disk-with-hole.jpg

My question is how I edit and set 0/D (boundary and initial conditions) for the case that (both time varying and non-time varying) uniform radial traction on the edge ("outer" patch of the model).
I intend to simulate a just-before-destruction by centrifugal force in a pseudo manner with this case.

Thank you for your attention in advance.