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Physics, 04.12.2019 00:31 alisonguerrero17

An aircraft component is fabricated from an aluminum alloy that has a plane strain fracture toughness of 39 . it has been determined that fracture results at a stress of 208 mpa when the maximum (or critical) internal crack length is 2.82 mm. a) determine the value of for this same component and alloy at a stress level of 270 mpa when the maximum internal crack length is 1.41 mm.

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