Engineering, 30.03.2020 15:09 lebronjames1604
Calculate the maximum internal crack length allowable for a Ti-6Al-4V titanium alloy component that is loaded to a stress one-half of its yield strength. Assume a yield strength 910 MPa, a plane strain fracture toughness of 55 MPa and that Y = 1.47. Enter your answer in accordance to the question statement mm
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Calculate the maximum internal crack length allowable for a Ti-6Al-4V titanium alloy component that...
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