Metal Forming Analysis

Calculate the strain distribution for the 1989 OSU benchmark test (Fig. 11.28), plane-strain version at punch heights of 20, 40, and 60 mm. Compare with benchmark results.
Assuming a Considere-type localization condition (i.e., necking begins at maximum load), what is the maximum punch height attainable in the plane-strain OSU benchmark test, shown in Fig. 11.28?
Imagine a uniform mesh of squares arranged in a rectangular array n m, where m > n. Assume that solver times and storage sizes (implicit, direct solution) can be approximated by
CPU(s) = K 1/ 250 db 2(s),
where d is the degrees of freedom (DOF), and b is the bandwidth (equal to the maximum number of degrees of freedom between adjacent nodes, however numbered); and
MB = 8/1000db(mb).
For fixed mesh dimensions of n = 50, m = 200, compare the CPU times and storage requirements for the following elements:
| membrane: | 3 DOF per node or 4 DOF per node, CFS |
| shell: | 6 DOF per node or 7 DOF per node, CFS |
| solid: | 3 DOF per node, 4 DOF for CFS in 1 element through-thickness |
| solid: | 3 DOF per node, 4 DOF for CFS in 25 elements through-thickness |
How would the CPU times and storage requirements change for each case in Part (a) if the nodes were numbered alternately?
Plot the CPU times and storage requirements for Part (a) if mesh refinement is carried out:
Part (a): n = 50, m...