The main contribution of the present work is the display of the impact of the addition of SiC into the aluminum alloy Al6061. For this reason, the Mode I stress intensity factor K(I) and T-stress for compact tension CT specimen are evaluated using 3D finite element analysis (FEA). The material used here in the compact tension CT specimen is Al6061-SiC metal matrix composites reinforced with various volume fractions of 4%, 6%, 10%, 12%, and 14% of SiC particles. Three different crack lengths (a/H) ratios of 0.35, 0.43, and 0.5 are considered through the analysis. Only half of the model of the cracked compact tension CT specimen with a subjected load of a magnitude Pâ=â603Â N is analyzed, and K(I), T(11)-stress, and T(33)-stress are computed. From the FEA results, it is observed that the K(I), T(11)-stress, and T(33)-stress are mainly influenced by the volume fractions of reinforced SiC particles. A more significant decrease in the values of K(I), T(11)-stress, and T(33)-stress is found in the Al6061-14vol.%SiC composite CT specimen. Where FEA results of K(I) for the Al6061-14vol.%SiC composite CT specimen exhibited reduction percentages of 5.4%, 5.6%, and 5.7%, respectively, for (a/H)â=â0.35, 0.43, and 0.5, as compared to those of Al6061. FEA values of T(11)-stress for the Al6061-14vol.%SiC composite CT specimen reduced by 5.5%, 5.6%, and 5.7%, respectively, for (a/H)â=â0.35, 0.43, and 0.5, respectively, over those of Al6061. Also, the decrement percentages of FEA results of T(33)-stress for the Al6061-14vol.%SiC composite CT specimen over those of Al6061 were found to be 17.1%, 16.6%, and 16.5%, respectively, for (a/H)â=â0.35, 0.43, and 0.5, respectively. Overall, fracture mechanics properties are improved by the addition of SiC particulates into the Al6061 alloy.
A study of fracture mechanics for compact tensile specimen of Al6061-SiC metal matrix composite.
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作者:Soliman, Ehab, Samir, Mohamed, Mohamed
| 期刊: | Scientific Reports | 影响因子: | 3.900 |
| 时间: | 2025 | 起止号: | 2025 Feb 17; 15(1):5763 |
| doi: | 10.1038/s41598-025-89041-w | ||
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