A component made of 7075-T6 aluminum alloy has an edge crack of 1.4 mm in length. Plane strain fracture toughness of this alloy is given as 27 MPA\M. Geometrical factor of the crack is given as 1.2. (a) If this alloy is subjected to uniaxial tensile stress of 380 MPa, determine whether sudder brittle fracture occurs or not. (b) Calculate the maximum allowable crack size for this component in order not to be failed ir brittle manner under a stress of 1000 MPa

Elements Of Electromagnetics
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Author:Sadiku, Matthew N. O.
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A component made of 7075-T6 aluminum alloy has an edge crack of 1.4 mm in length. Plane
strain fracture toughness of this alloy is given as 27 MPaym. Geometrical factor of the crack
is given as 1.2.
(a) If this alloy is subjected to uniaxial tensile stress of 380 MPa, determine whether sudden
brittle fracture occurs or not.
(b) Calculate the maximum allowable crack size for this component in order not to be failed in
brittle manner under a stress of 1000 MPa
Transcribed Image Text:A component made of 7075-T6 aluminum alloy has an edge crack of 1.4 mm in length. Plane strain fracture toughness of this alloy is given as 27 MPaym. Geometrical factor of the crack is given as 1.2. (a) If this alloy is subjected to uniaxial tensile stress of 380 MPa, determine whether sudden brittle fracture occurs or not. (b) Calculate the maximum allowable crack size for this component in order not to be failed in brittle manner under a stress of 1000 MPa
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