Engineering, 01.06.2020 16:57 john3195
A structural component is fabricated from an alloy that has a plane-strain fracture toughness of 62 MPa√m. It has been determined that this component fails at a stress of 250 MPa when the maximum length of an internal crack is 1.6 mm. What is the maximum allowable internal crack length (in mm) without fracture for this same component exposed to a stress of 250 MPa and made from another alloy that has a plane strain fracture toughness of 40 MPa√m?
Answers: 2
Engineering, 04.07.2019 16:10
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Engineering, 04.07.2019 16:10
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Engineering, 04.07.2019 18:10
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Engineering, 04.07.2019 18:10
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A structural component is fabricated from an alloy that has a plane-strain fracture toughness of 62...
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