1. For the tensile member shown in Figure P7–25 on the next page with two holes, determine the…


1. For the tensile component shown in Figure P7–25 on the direct page after a while two holes, particularize the completion foremost stresses and their locations. Let E = 210 GPa, n = 0:25, and t = 10 mm. Then let E = 70 GPa and n = 0:30. Compare your results. Use 20 kN unfurl uninterruptedly aggravate the suitable edge.

2. For the concoction shown in Figure P7–26 on the direct page, particularize the completion foremost stresses and their locations. Let E = 210 GPa and v = 0:25.