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The critical point of a plane stress design has principal stresses of $1 = 21 kpsi and s = -7 kpsi. Were the designed
The critical point of a plane stress design has principal stresses of $1 = 21 kpsi and s = -7 kpsi. Were the designed component made of a brittle material with an ultimate tensile strength of 30 kpsi and an ultimate compressive strength of 80 kpsi, the safety factor based on the Modified Mohr static failure criterion would be about: 1.4 11.4 3.8 4.3 1.9
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