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 √/m and that Y= 1.47.

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 √/m and that Y= 1.47.

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

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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 MPam and that Y = 1.47.
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