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GE_Jet engine bracket challenge_1

GE_Jet engine bracket challenge_1

grabcad

In our analysis, the mass of the component is 0.95 g, representing a 55% approximate reduction in weight. FEA results depict performance under three load scenarios. However, we noticed that optimal outcomes were not achieved when weight reduction exceeded 40%, an observation common to other entries. As a result, we're concentrating on a heavier but safer part design.

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