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Physics, 14.11.2019 02:31 annamariaafowyhrq

Awing component on an aircraft is fabricated from an aluminum alloy that has a plane strain fracture toughness of 26 mpa√m . it has been determined that the fracture results at a stress of 112 mpa when the maximum internal crack length is 8.6 mm. for this same component and alloy, compute the stress level at which fracture will occur for a critical internal crack length of 6.0 mm

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