Engineering, 11.03.2020 18:30 djmelodiedaniels
An aircraft component is fabricated from an aluminum alloy that has a plane strain fracture toughness of 37 MPam. It has been determined that fracture results at a stress of 206 MPa when the maximum (or critical) internal crack length is 2.58 mm. a) Determine the value of Yσπa for this same component and alloy at a stress level of 267 MPa when the maximum internal crack length is 1.29 mm.
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An aircraft component is fabricated from an aluminum alloy that has a plane strain fracture toughnes...
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