Micromechanical modeling of fracture initiation in 7050 aluminum |
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Authors: | Michael R. Hill Tina L. Panontin |
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Affiliation: | a Department of Mechanical and Aeronautical Engineering, University of California, Davis, CA 95616-5294, USA b Chief Engineer, NASA-Ames Research Center, Moffett Field, CA 94035-1000, USA |
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Abstract: | Mechanical testing and finite element calculations have been carried out to characterize the fracture initiation behavior of the high-strength aluminum alloy 7050-T7451. Results show that fracture initiation is well predicted for two specimen types of differing constraint using the stress-modified, critical plastic strain micromechanical model. The relation between stress triaxiality and critical plastic strain was found from a series of notched tensile specimens. Data from these tests are interpreted using both companion finite element modeling and common, semi-empirical relations, and these two approaches are compared. Multiple, interrupted tests of standard, highly constrained single edge notched bend specimens are used to obtain the J–R curve in 7050 for small amounts of tearing to experimentally identify initiation. Companion modeling and the stress-modified, critical plastic strain relation are used to find the length scale for fracture, l*, needed for initiation predictions. The calibrated stress-modified, critical plastic strain relation and length scale are then used to predict fracture initiation of a low-constraint specimen. The prediction is within 5% of the experimental measurements. Finally, various aspects of the procedure followed in the present work are compared to previous efforts using similar approaches. |
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Keywords: | Fracture Aluminum Micromechanical modeling Constraint |
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