StructuralFEA
Structural
- Sep 18, 2015
- 23
I have modeled a vehicle carrier using solids and shells in FEMAP. I refined the mesh for the shells twice, and the solution converged, i.e. became asymptotic. However, I find the last few elements near the interface between a round HSS, and a square HSS to be have very high stresses. How do I make sure that these stresses/numbers are correct? As you can see, I have already run a convergence analysis. I have also compared the minimum, average, and maximum nodal Von Mises stresses to see the percent difference. Despite convergence of the analysis, the difference between minimum and average stresses, or between average and maximum stresses, is sometimes as high as 28%. Are these stresses reliable?
Thanks.
Thanks.