碳纤维复合靶板抗破片冲击性能研究OA北大核心CSTPCD
Study on Anti-Fragment Impact Performance of Carbon Fiber Reinforced Plastics
为探究碳纤维复合材料的抗破片侵彻性能,进行了 8g立方体钢破片侵彻厚度分别为5、10、15 mm碳纤维复合材料靶板试验,获取破片着靶速度,并回收破片、靶板,观测靶板破坏情况.根据试验情况进行数值模拟,探究破片侵彻碳纤维复合材料靶板的过程及碳纤维复合材料靶板的破坏机理,由此得到靶板破坏形式与破片速度的关系:破片速度大于弹道极限时,靶板以纤维的剪切破坏为主;破片速度逐渐降低时,纤维的拉伸破坏、基体破裂与纤维层分层多种破坏形式所占比重随着破片速度的变化而变化.
In order to explore the anti-penetration property of carbon fiber composite materials,a series of experiments need to be carried out.In experiments,8 g cubic steel fragments penetrated carbon fiber reinforced plastics whose thickness are 5,10 and 15 mm respectively.The velocity of fragments was obtained,the situation of target was observed,fragments and carbon fiber were recovered.The numerical simulations were carried out according to the situation of experiments.The process of fragments penetrating carbon fiber composite target was explored,and the failure mechanism of carbon fiber composite target was also explored.The relationship between the failure mode and velocity of fragments could be described as follows:when the fragment velocity exceeds the ballistic limit,the main form of target damage is fiber shear failure;when the fragment velocity is lower than the ballistic limit,the damage forms of the target include fiber shear failure,fiber tensile failure,matrix cracking and fiber layer delamination,and their proportions change with the fragment velocity.
李巧歌;梁增友;王春光;郝永强
中北大学机电工程学院,山西 太原 030051晋西集团江阳公司,山西 太原 030051内蒙动力机械研究所,内蒙古 呼和浩特 010000
力学
碳纤维复合材料弹道侵彻试验破片破坏机理
carbon fiber reinforced plasticsballistic penetration testfragmentfailure mechanism
《高压物理学报》 2024 (004)
90-99 / 10
山西省科技厅省基础研究计划项目(202103021224210)
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