Solve the following problems using a computer program. In some of these problems, we suggest that students be assigned separate parts (or models) to facilitate parametric studies.
Determine the stresses in the plate shown in Figure P7–30 on page 431. Let E = 210 GPa and v = 0.25. The element thickness is 10 mm.
for the upper part. The part is made of 6061 aluminum alloy. Is the thickness sufficient to prevent failure based on the maximum distortion energy theory? If not, suggest a better thickness. (Scale all dimensions as needed.)
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