2020
DOI: 10.1016/j.tafmec.2020.102760
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On the mixed mode I/II/III translaminar fracture toughness of cotton/epoxy laminated composites

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Cited by 17 publications
(6 citation statements)
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“…Table 1 shows the mechanical properties of the PMMA sheet utilized in this study, for which testing was conducted in accordance with ASTM D638 and D732 standards. Numerous testing methods and specimens, such as incline edge crack asymmetric bending [ 3 ], compact tension shear [ 6 ], asymmetric four-point bending [ 22 ], semi-circular bending [ 23 ], Brazilian disc specimen [ 24 ], etc., are used to study mixed-mode I/II fracture toughness. In this study, the mixed-mode I/II of PMMA was studied using the inclined crack bending specimen based on previous research by Mingdong Wei [ 25 ] and M.R.M.…”
Section: Mixed-mode I/ii Fracture Toughnessmentioning
confidence: 99%
See 1 more Smart Citation
“…Table 1 shows the mechanical properties of the PMMA sheet utilized in this study, for which testing was conducted in accordance with ASTM D638 and D732 standards. Numerous testing methods and specimens, such as incline edge crack asymmetric bending [ 3 ], compact tension shear [ 6 ], asymmetric four-point bending [ 22 ], semi-circular bending [ 23 ], Brazilian disc specimen [ 24 ], etc., are used to study mixed-mode I/II fracture toughness. In this study, the mixed-mode I/II of PMMA was studied using the inclined crack bending specimen based on previous research by Mingdong Wei [ 25 ] and M.R.M.…”
Section: Mixed-mode I/ii Fracture Toughnessmentioning
confidence: 99%
“…For the majority of engineering parts, the load pattern or direction is more likely to occur in a mixed direction than in just one direction. According to the nature of the load direction on that part, it must be studied in a mixed-mode fracture toughness; either it is studied in mixed-mode I/II [ 2 , 3 ], mixed-mode I/III [ 4 , 5 ], or mixed-mode II/III [ 6 , 7 ], with mixed-mode I/II loading being popularly studied in various research. The fracture toughness values under mixed-mode loading can be calculated under several methods such as actual testing, numerical method, etc.…”
Section: Introductionmentioning
confidence: 99%
“…Although attempts were made to improve it, including blending with high-toughness thermoplastic materials such composites cannot easily be recycled. [4][5][6][7][8] Due to the increase in electromagnetic (EM) waves generating electronic devices onboard aircraft, electromagnetic interference (EMI) shielding by surrounding devices is another challenge for commercial and military aircraft to safely work devices. [9][10][11] For stealth applications, a reduction in radar cross section (RCS), a measure of detectability by radar, is required.…”
Section: Introductionmentioning
confidence: 99%
“…On the other hand, thermosets such as epoxy have another disadvantage of low fracture toughness due to their brittle nature caused by their cross‐linked molecular chain structure. Although attempts were made to improve it, including blending with high‐toughness thermoplastic materials such composites cannot easily be recycled 4–8 . Due to the increase in electromagnetic (EM) waves generating electronic devices onboard aircraft, electromagnetic interference (EMI) shielding by surrounding devices is another challenge for commercial and military aircraft to safely work devices 9–11 .…”
Section: Introductionmentioning
confidence: 99%
“…This type of failure, like the others, may be caused under different loading conditions. Based on the direction of loading, mode I, mode II, and mode III translaminar fracture or any combination of them may occur in the laminated composites [10]. Most of researchers have studied the translaminar fracture behavior of laminated composites under mode I loading condition [11][12][13][14][15][16].…”
Section: Introductionmentioning
confidence: 99%