Guru's,
I need to run an analysis of a part that has a fairly complicated
assembly bolted up to it. I don't want to run the assembly in the
analysis due to complexity, but I want to capture it's effect on the
part in question. I believe I can do this by modeling a "point mass
load" at the assemblies CG with the load equal to it's weight and then
connecting this with rigids to the bolt holes. I'm not sure if this is
the best approach. Anyone have any guidelines, recommended practices?
Thanks...
Paul Korenkiewicz
FEV, Inc.
4554 Glenmeade
Auburn Hills, MI., 48326
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