2023
DOI: 10.1016/j.ijmecsci.2022.108057
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The influence of pin on the low-velocity impact performance of foam sandwich structure

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Cited by 17 publications
(4 citation statements)
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“…However, most of these studies focused on the case of quasi-static loads, including indentation [ 25 , 26 ], three-point bending [ 27 , 28 , 29 ], energy absorption [ 30 , 31 , 32 , 33 ], and damage and fatigue [ 34 , 35 , 36 ]. Compared with research on sandwich structures with PMI foam cores under quasi-static loads, studies on the dynamic response of PMI foam sandwich structures are few [ 37 , 38 , 39 , 40 , 41 ]. Yang et al [ 38 ] studied the geometric scale effect on the dynamic response of sandwich panels with PMI foam cores.…”
Section: Introductionmentioning
confidence: 99%
“…However, most of these studies focused on the case of quasi-static loads, including indentation [ 25 , 26 ], three-point bending [ 27 , 28 , 29 ], energy absorption [ 30 , 31 , 32 , 33 ], and damage and fatigue [ 34 , 35 , 36 ]. Compared with research on sandwich structures with PMI foam cores under quasi-static loads, studies on the dynamic response of PMI foam sandwich structures are few [ 37 , 38 , 39 , 40 , 41 ]. Yang et al [ 38 ] studied the geometric scale effect on the dynamic response of sandwich panels with PMI foam cores.…”
Section: Introductionmentioning
confidence: 99%
“…As shown in Figure 5a,c, the loading and unloading parts of the curves of specimens A-1 and B-1 are smooth (the slight nonlinearity is caused by geometric nonlinearity during the impact process) without any slope change, indicating that no significant damage or cracking occurred in the face layer during the impact process. However, in Figure 5b,d, the initial parts of the stress-strain curves of specimens A-2 and B-2 are linear, corresponding to the linear elastic behavior of the core foam before the face layer is damaged [26]. As the strain continued to increase, the stress suddenly decreased, indicating the cracking of the face panel.…”
Section: Low-speed Impact Performancementioning
confidence: 95%
“…As the strain continued to increase, the stress suddenly decreased, indicating the cracking of the face panel. As the hammer continued to move However, in Figure 5b,d, the initial parts of the stress-strain curves of specimens A-2 and B-2 are linear, corresponding to the linear elastic behavior of the core foam before the face layer is damaged [26]. As the strain continued to increase, the stress suddenly decreased, indicating the cracking of the face panel.…”
Section: Low-speed Impact Performancementioning
confidence: 95%
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