2022
DOI: 10.3390/met12050785
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Effect of Surface Mechanical Attrition Treatment on Torsional Fatigue Properties of a 7075 Aluminum Alloy

Abstract: The effect of Surface Mechanical Attrition Treatment (SMAT) on torsional fatigue properties of a 7075 aluminum alloy was investigated. A number of fatigue samples were heat treated to increase the sensitivity of the material to SMAT. Compared with the as-machined (AM) samples, the fatigue lives of their SMATed counterparts (AM-SMAT) tested under torsional loading increased under high stress amplitudes, but decreased under low amplitudes. However, the fatigue lives of heated and SMATed samples (HT-SMAT) increas… Show more

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Cited by 7 publications
(6 citation statements)
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“…Mechanical changes in the material are indicated by a decrease in the modulus of the material under plastic strain [34]. Several parameters affect the fatigue life: the applied load, surface area, and fatigue [35]. The applied load significantly affects the fatigue life of porous magnesium.…”
Section: Discussionmentioning
confidence: 99%
“…Mechanical changes in the material are indicated by a decrease in the modulus of the material under plastic strain [34]. Several parameters affect the fatigue life: the applied load, surface area, and fatigue [35]. The applied load significantly affects the fatigue life of porous magnesium.…”
Section: Discussionmentioning
confidence: 99%
“…SMAT has been employed recently to induce nanocrystalline surface layers and gradient nanostructures in different alloys. [13][14][15][16] The SMAT effect on a 7075-aluminum alloy's torsional fatigue behavior was studied by Li et al [15] The results demonstrated that SMAT could have positive and negative effects on fatigue life, depending on the testing conditions, where factors such as surface roughness, grain refinement and residual stresses affected the results. Applying SMAT leads to a substantial reduction in grain size to the nanoscale within the alloy's surface layer, where the grain size progressively increases from the surface to the core of the material.…”
Section: Doi: 101002/adem202300549mentioning
confidence: 99%
“…[13,42] Such a nonuniform distribution of the microstructural features generates a hardness gradient in the SMATed layer (Figure 11, 12, 14, and19a). Nanomechanical behavior also shows a gradient nature due to the gradient microstructure (Figure [13][14][15][16][17][18]. Attrition of AZ91D specimen surface with higher velocity balls (e.g., %10 m s À1 ) is useful in forming a considerably thicker layer (%3500 μm) with higher hardness (%2 GPa at the surface) and compressive stress (about À281 MPa (max.)…”
Section: Srssmentioning
confidence: 99%
“…The Basquin equation is commonly used to model the fatigue data trend for different numbers of cycles by using the statistical calculation of the S-N curves (Figure 10). The Basquin equation has the form [45][46][47][48][49][50][51][52][53][54][55][56][57]:…”
Section: Fatigue Life Before Corrosion After Corrosionmentioning
confidence: 99%