2008
DOI: 10.1016/j.ijfatigue.2007.01.056
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Modelling the high-temperature longitudinal fatigue behaviour of metal matrix composites (SiC/Ti-6242): Nonlinear time-dependent matrix behaviour

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Cited by 16 publications
(2 citation statements)
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“…Quast et al [ 13 ] investigated the out-of-phase thermomechanical fatigue behavior of Ultra SCS-6/Ti-24Al-17Nb-xMo (at.%) MMCs; the fatigue behavior of two 2009/SiC/15p-T4 DRA (discontinuously reinforced aluminum) composites in the very high cycle fatigue was investigated by Huang et al [ 14 ]; Ni et al [ 15 ] studied residual stresses and high cycle fatigue properties of friction stir welded SiCp/AA2009 composites; fatigue failure mechanisms of microsphere Al2O3-Al particulate MMCs were determined from examination of the fracture surfaces and the crack profiles by Park et al [ 16 ]; Sivananth et al [ 7 ] evaluated the load bearing behavior of titanium carbide reinforced aluminum matrix composites and their suitability for automotive application; Feng et al [ 17 ] determined the relationship between the applied stress and fatigue life of a SiC fiber-reinforced titanium matrix composite and examined the fracture surfaces to study the fatigue damage and fracture failure mechanisms using SEM; and the creep–fatigue behavior of aluminum alloy-based MMC has been modeled using an idealized plane strain model [ 18 ]. Moreover, many other related studies may be found in [ 19 , 20 , 21 , 22 , 23 , 24 , 25 ].…”
Section: Introductionmentioning
confidence: 99%
“…Quast et al [ 13 ] investigated the out-of-phase thermomechanical fatigue behavior of Ultra SCS-6/Ti-24Al-17Nb-xMo (at.%) MMCs; the fatigue behavior of two 2009/SiC/15p-T4 DRA (discontinuously reinforced aluminum) composites in the very high cycle fatigue was investigated by Huang et al [ 14 ]; Ni et al [ 15 ] studied residual stresses and high cycle fatigue properties of friction stir welded SiCp/AA2009 composites; fatigue failure mechanisms of microsphere Al2O3-Al particulate MMCs were determined from examination of the fracture surfaces and the crack profiles by Park et al [ 16 ]; Sivananth et al [ 7 ] evaluated the load bearing behavior of titanium carbide reinforced aluminum matrix composites and their suitability for automotive application; Feng et al [ 17 ] determined the relationship between the applied stress and fatigue life of a SiC fiber-reinforced titanium matrix composite and examined the fracture surfaces to study the fatigue damage and fracture failure mechanisms using SEM; and the creep–fatigue behavior of aluminum alloy-based MMC has been modeled using an idealized plane strain model [ 18 ]. Moreover, many other related studies may be found in [ 19 , 20 , 21 , 22 , 23 , 24 , 25 ].…”
Section: Introductionmentioning
confidence: 99%
“…The course of the deformation process in the conditions of simultaneous action of a variable temperature and of mechanical and thermal loads has been described in many papers concerning solid body mechanics. Some papers attempted to generalise the description of the behaviour of materials through constitutive equations for complex stress states that take into account rheological phenomena and dependencies of material properties on the temperature, including Leimatre and Chaboche models [1][2][3] which are commonly used to describe the properties of materials applied for operation at an elevated temperature or, for example the model of Kichenin and co-authors [3] or the one developed by Figiel and Günter [4]. Therefore, this paper naturally is not an attempt at such generalisation.…”
Section: Introductionmentioning
confidence: 99%