Design a material and its treatment

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Reference no: EM131274603

A part for an engine mount for a private aircraft must occupy a volume of 60 cm³ with a minimum thickness of 0.5 cm and a minimum width of 4 cm. The load on the part during service may be as much as 75,000 N. The part is expected to remain below 100°C during service. Design a material and its treatment that will perform satisfactorily in this application.

Reference no: EM131274603

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