2002
DOI: 10.1016/s1359-6454(01)00401-3
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Changes in the misfit stresses in an Al/SiCp metal matrix composite under plastic strain

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Cited by 58 publications
(35 citation statements)
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“…The values are consistent with thosem easured previously, [7,28] at around 70 MPa in the matrix and -340 MPa in the reinforcement.A st he composite is loaded elastically,t here is initially no change in the misfit stress:t his justifies the use of an aspect ratio of 1.6, as am iscalculation of the elastic load transfer would manifest itselfa savariation in the calculated misfit stress during elastic loading (even a change of 0.1 in the aspectratio does produce ameasurable difference in the results). The misfit stress should remain constant unless there is achange in temperature or the onset of plastic effects.…”
Section: Stress Separationsupporting
confidence: 93%
“…The values are consistent with thosem easured previously, [7,28] at around 70 MPa in the matrix and -340 MPa in the reinforcement.A st he composite is loaded elastically,t here is initially no change in the misfit stress:t his justifies the use of an aspect ratio of 1.6, as am iscalculation of the elastic load transfer would manifest itselfa savariation in the calculated misfit stress during elastic loading (even a change of 0.1 in the aspectratio does produce ameasurable difference in the results). The misfit stress should remain constant unless there is achange in temperature or the onset of plastic effects.…”
Section: Stress Separationsupporting
confidence: 93%
“…Metal matrix composites are well-known to generate internal residual stresses in the two phases, because of the difference in coefficient of thermal expansion (CTE) of the matrix and reinforcement [12][13][14]. For an Al-SiC system with 20% SiC partlices, where the matrix has a CTE around five times higher than the reinforcement (~4.5 µε/K compared with 23.4 µε/K), typical residual stresses at room temperature arising from the shape misfits are +70 MPa in the matrix and -280 MPa in the reinforcement [13].…”
Section: Introductionmentioning
confidence: 99%
“…However, during the manufacturing and subsequently heat treatments, tensile stresses are always generated [1]. As the formed tensile stresses may deteriorate the fatigue properties, it is therefore of interest to apply a mechanical surface treatment to change the unfavorable stress state [4]. As an effective and important surface treatment method, shot peening (SP) can considerably improve fatigue strength and fatigue life of cyclically loaded metallic components by inducing compressive residual stress (CRS) and work hardening into the surface region [5].…”
Section: Introductionmentioning
confidence: 99%