Experimental and Numerical Investigation of the Tensile and Failure Response of Multiple-Hole-Fiber-Reinforced Magnesium Alloy Laminates under Various Temperature Environments
In this paper, the tensile mechanical behavior and progressive damage morphology of glass-fiber-reinforced magnesium alloy laminate for different numbers of holes in a temperature range of 25–180 °C were investigated. In addition, based on extensive tensile tests, the tensile mechanical behavior and...
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author | Zhongzhao Lin Dongfa Sheng Yuting Fang Ke Xiong Yuming Song |
author_facet | Zhongzhao Lin Dongfa Sheng Yuting Fang Ke Xiong Yuming Song |
author_sort | Zhongzhao Lin |
collection | DOAJ |
description | In this paper, the tensile mechanical behavior and progressive damage morphology of glass-fiber-reinforced magnesium alloy laminate for different numbers of holes in a temperature range of 25–180 °C were investigated. In addition, based on extensive tensile tests, the tensile mechanical behavior and microscopic damage morphology of porous-glass-fiber-reinforced magnesium alloy laminates at different temperatures were observed by finite element simulation and scanning electron microscopy (SEM). Finally, the numerical simulation and experimental results were in good accordance with the prediction of mechanical properties and fracture damage patterns of the laminates, the average difference between the residual strength values of the specimens at ambient temperature was 5.57%, and the stress–strain curves were in good agreement. The experimental and finite element analysis results showed that the damaged area of the bonded layer tended to expand with the increase in the number of holes, which has a lesser effect on the ultimate tensile strength. As the temperature increased, the specimens changed from obvious fiber breakage (pull-out) and the resin matrix damage mode to matrix softening damage and interfacial delamination fracture damage. As the testing temperature of the specimens increased from 25 °C to 180 °C, the tensile strength of the specimens decreased by an average of 51.59%, while the tensile strength of the specimens showed a nonlinear decreasing trend. The damage mechanism of porous-glass-fiber-reinforced magnesium alloy laminates at different temperatures is discussed in this paper, which can provide a reference for engineering applications and design. |
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language | English |
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spelling | doaj.art-ac7e650327514415a13762469f66f7ce2023-11-19T01:59:34ZengMDPI AGMaterials1996-19442023-08-011616557310.3390/ma16165573Experimental and Numerical Investigation of the Tensile and Failure Response of Multiple-Hole-Fiber-Reinforced Magnesium Alloy Laminates under Various Temperature EnvironmentsZhongzhao Lin0Dongfa Sheng1Yuting Fang2Ke Xiong3Yuming Song4School of Civil Engineering, Southwest Forestry University, Kunming 650224, ChinaSchool of Civil Engineering, Southwest Forestry University, Kunming 650224, ChinaSchool of Civil Engineering, Southwest Forestry University, Kunming 650224, ChinaNational Supercomputing Center in Guangzhou, Sun Yat-Sen University, Guangzhou 510006, ChinaSchool of Chemistry and Chemical Engineering, Kunming University, Kunming 650214, ChinaIn this paper, the tensile mechanical behavior and progressive damage morphology of glass-fiber-reinforced magnesium alloy laminate for different numbers of holes in a temperature range of 25–180 °C were investigated. In addition, based on extensive tensile tests, the tensile mechanical behavior and microscopic damage morphology of porous-glass-fiber-reinforced magnesium alloy laminates at different temperatures were observed by finite element simulation and scanning electron microscopy (SEM). Finally, the numerical simulation and experimental results were in good accordance with the prediction of mechanical properties and fracture damage patterns of the laminates, the average difference between the residual strength values of the specimens at ambient temperature was 5.57%, and the stress–strain curves were in good agreement. The experimental and finite element analysis results showed that the damaged area of the bonded layer tended to expand with the increase in the number of holes, which has a lesser effect on the ultimate tensile strength. As the temperature increased, the specimens changed from obvious fiber breakage (pull-out) and the resin matrix damage mode to matrix softening damage and interfacial delamination fracture damage. As the testing temperature of the specimens increased from 25 °C to 180 °C, the tensile strength of the specimens decreased by an average of 51.59%, while the tensile strength of the specimens showed a nonlinear decreasing trend. The damage mechanism of porous-glass-fiber-reinforced magnesium alloy laminates at different temperatures is discussed in this paper, which can provide a reference for engineering applications and design.https://www.mdpi.com/1996-1944/16/16/5573fiber metal laminatesmultiple holestemperature effecttensile responsenumerical simulationdamage evolution |
spellingShingle | Zhongzhao Lin Dongfa Sheng Yuting Fang Ke Xiong Yuming Song Experimental and Numerical Investigation of the Tensile and Failure Response of Multiple-Hole-Fiber-Reinforced Magnesium Alloy Laminates under Various Temperature Environments Materials fiber metal laminates multiple holes temperature effect tensile response numerical simulation damage evolution |
title | Experimental and Numerical Investigation of the Tensile and Failure Response of Multiple-Hole-Fiber-Reinforced Magnesium Alloy Laminates under Various Temperature Environments |
title_full | Experimental and Numerical Investigation of the Tensile and Failure Response of Multiple-Hole-Fiber-Reinforced Magnesium Alloy Laminates under Various Temperature Environments |
title_fullStr | Experimental and Numerical Investigation of the Tensile and Failure Response of Multiple-Hole-Fiber-Reinforced Magnesium Alloy Laminates under Various Temperature Environments |
title_full_unstemmed | Experimental and Numerical Investigation of the Tensile and Failure Response of Multiple-Hole-Fiber-Reinforced Magnesium Alloy Laminates under Various Temperature Environments |
title_short | Experimental and Numerical Investigation of the Tensile and Failure Response of Multiple-Hole-Fiber-Reinforced Magnesium Alloy Laminates under Various Temperature Environments |
title_sort | experimental and numerical investigation of the tensile and failure response of multiple hole fiber reinforced magnesium alloy laminates under various temperature environments |
topic | fiber metal laminates multiple holes temperature effect tensile response numerical simulation damage evolution |
url | https://www.mdpi.com/1996-1944/16/16/5573 |
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