Physics, 03.12.2019 19:31 paiged2003
Problem 9.10 calculate the maximum internal crack length allowable for a 2024-t3 aluminum alloy component that is loaded to a stress one-half of its yield strength. assume a yield strength 345 mpa, a plane strain fracture toughness of 44 mpa and that y = 1.53.
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Problem 9.10 calculate the maximum internal crack length allowable for a 2024-t3 aluminum alloy comp...
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