Question: Task 2 Some aluminum aircraft components have a K lc = 35 MPa (m) 1/2 . It has been determined that the breach occurs at

Task 2 Some aluminum aircraft components have a Klc = 35 MPa (m)1/2. It has been determined that the breach occurs at a stress of 250 MPa when the critical internal crack length is 2 mm. Will this component achieve breakage at a voltage of 325MPa reaches critical internal crack length is 1.1 mm?

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