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低速冲击激励下嵌入黏弹性阻尼芯层的纤维金属混杂层合板动态响应预测模型

李则霖 李晖 王东升 任朝晖 祖旭东 周晋 官忠伟 王相平

李则霖, 李晖, 王东升, 任朝晖, 祖旭东, 周晋, 官忠伟, 王相平. 低速冲击激励下嵌入黏弹性阻尼芯层的纤维金属混杂层合板动态响应预测模型[J]. 力学学报, 2020, 52(6): 1690-1699. doi: 10.6052/0459-1879-20-165
引用本文: 李则霖, 李晖, 王东升, 任朝晖, 祖旭东, 周晋, 官忠伟, 王相平. 低速冲击激励下嵌入黏弹性阻尼芯层的纤维金属混杂层合板动态响应预测模型[J]. 力学学报, 2020, 52(6): 1690-1699. doi: 10.6052/0459-1879-20-165
Li Zelin, Li Hui, Wang Dongsheng, Ren Chaohui, Zu Xudong, Zhou Jin, Guan Zhongwei, Wang Xiangping. A DYNAMIC RESPONSE PREDICTION MODEL OF FIBER-METAL HYBRID LAMINATED PLATES EMBEDDED WITH VISCOELASTIC DAMPING CORE UNDER LOW-VELOCITY IMPACT EXCITATION[J]. Chinese Journal of Theoretical and Applied Mechanics, 2020, 52(6): 1690-1699. doi: 10.6052/0459-1879-20-165
Citation: Li Zelin, Li Hui, Wang Dongsheng, Ren Chaohui, Zu Xudong, Zhou Jin, Guan Zhongwei, Wang Xiangping. A DYNAMIC RESPONSE PREDICTION MODEL OF FIBER-METAL HYBRID LAMINATED PLATES EMBEDDED WITH VISCOELASTIC DAMPING CORE UNDER LOW-VELOCITY IMPACT EXCITATION[J]. Chinese Journal of Theoretical and Applied Mechanics, 2020, 52(6): 1690-1699. doi: 10.6052/0459-1879-20-165

低速冲击激励下嵌入黏弹性阻尼芯层的纤维金属混杂层合板动态响应预测模型

doi: 10.6052/0459-1879-20-165
基金项目: 1) 国家自然科学基金(51505070);国家自然科学基金(51970530);国家自然科学基金(U1708257);中央高校基本科研业务费专项资金(N160313002);中央高校基本科研业务费专项资金(N160312001);中央高校基本科研业务费专项资金(N170302001);中央高校基本科研业务费专项资金(N180302004);中央高校基本科研业务费专项资金(N180703018);中央高校基本科研业务费专项资金(N180312012);中央高校基本科研业务费专项资金(N180313006);装备预研重点实验室基金(6142905192512)
详细信息
    作者简介:

    2) 李晖,副教授,研究方向:复合材料结构动力学. E-mail: lh200300206@163.com

    通讯作者:

    李晖

  • 中图分类号: V257,O313.4

A DYNAMIC RESPONSE PREDICTION MODEL OF FIBER-METAL HYBRID LAMINATED PLATES EMBEDDED WITH VISCOELASTIC DAMPING CORE UNDER LOW-VELOCITY IMPACT EXCITATION

  • 摘要: 本文首次从解析角度建立了低速冲击激励下嵌入黏弹性阻尼芯层的纤维金属混杂层合板动态响应预测模型. 首先,结合经典层合板理论和冯$\cdot$卡门假设,建立了嵌入黏弹性芯层的纤维金属混杂层合板弹性损伤本构关系. 然后,将层合板受冲击时的变形分成接触和拉伸两个区域,在接触区域内,对金属层采用 Von Mises 失效准则,纤维层采用 Tsai-Hill 失效准则和对黏弹性层采用指数 Drucker-Prager 失效准则判断层合板损伤情况. 考虑不同材料层对冲击动态响应的贡献来修正两个变形区域的位移公式,进而计算结构因弹性变形产生的应变能,以及接触区域因塑性变形消耗的能量,实现每次失效事件发生后各层材料的能量、位移和冲击接触力的理论求解,并给出了结构动态响应分析的具体流程图. 最后,以嵌入 Zn33 黏弹性芯层的 TA2 钛合金混杂 T300 碳纤维/树脂层合板为研究对象,开展落锤冲击实验. 验证结果表明,理论预测与测试获得的冲击接触力、位移响应以及冲击载荷-位移曲线吻合较好,且关注的峰值点计算误差最大不超过 9%,进而验证了所提出的理论模型的有效性.

     

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  • 收稿日期:  2020-05-16
  • 刊出日期:  2020-12-10

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