The influence of matrix microstructure |
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Authors: | G. M. Vyletel J. E. Allison D. C. Aken |
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Affiliation: | (1) Johnson Controls, Inc., 48170 Plymouth, MI;(2) Ford Research Laboratory, Ford Motor Company, 48121 Dearborn, MI;(3) University of Missouri-Rolla, 65401 Rolla, MO |
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Abstract: | The low-cycle and high-cycle fatigue behavior and cyclic response of naturally aged and artificially aged 2219/TiC/15p and unreinforced 2219 Al were investigated utilizing plastic strain-controlled and stress-controlled testing. The cyclic response of both the reinforced and un-reinforced materials was similar for all plastic strain amplitudes tested except that the saturation stress level for the composite was always greater than that of the unreinforced material. The cyclic response of the naturally aged materials exhibited cyclic hardening and, in some cases, cyclic softening, while the cyclic response for the artificially aged materials showed no evidence of either cyclic hardening or softening. The higher ductility of the unreinforced material made it more resistant to fatigue failure at high strains, and thus, at a given plastic strain, it had longer fatigue life. It should be noted that the tensile ductilities of the 2219/TiC/15p were significantly higher than those previously reported for 2XXX-series composites. During stress-controlled test-ing at stresses below 220 MPa, the presence of TiC particles lead to an improvement in fatigue life. Above 220 MPa, no influence of TiC reinforcement on fatigue life could be detected. In both the composite and unreinforced materials, the low-cycle and high-cycle fatigue lives were found to be virtually independent of matrix microstructure. G.M. VYLETEL, formerly Graduate Student, Department of Materials Science and Engineering, The University of Michigan D.C. VAN AKEN, formerly Assistant Professor, Department of Materials Science and Engineering, The University of Michigan |
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