In the attached assembly model file, I am only interested in stresses on the shaft. In order to reduce the global mesh size I would like to replace the fan, the motor, and the stator with point masses and apply mass moment of inertias and other boundary conditions associated with them. I know there is a "new mass" B.C. option in the Mecway CCX solver that we could use.
Motor and shaft have steel properties and rotor and stator have nylon nylon material.
I need guidance on how to setup the point masses and apply B.C's.
Any help would be appreciated.
Comments
For a remote mass with CCX, you can use node-surface coupling and put a mass on the reference node.
Thanks
It might be easier to make simplified solid parts that have the required properties, or maybe just use a very coarse mesh for the existing parts.