• 首页 | 期刊简介 | 编委会 | 投稿须知 | 出版道德规范 | 下载专区 | English
李志斌.夹芯板结构局部压入力学响应研究[J].实验力学,2016,31(2):277~282
夹芯板结构局部压入力学响应研究
On the Mechanical Response of Local Indentation for a Sandwich Panel Structure
投稿时间:2014-08-21  修订日期:2015-08-25
DOI:10.7520/1001-4888-14-160
中文关键词:  夹芯板  压入  泡沫铝  无量纲参数
英文关键词:sandwich panel  indentation  foamed aluminum  dimensionless parameter
基金项目:国家自然科学基金(11402299)资助
作者单位
李志斌 国防科学技术大学理学院 湖南长沙 410073 
摘要点击次数: 738
全文下载次数: 612
中文摘要:
      利用材料试验机(MTS)实验研究了复合材料面板、闭孔泡沫铝芯层夹芯板结构在准静态压入时的变形和破坏特征。实验结果表明,夹芯板的破坏主要集中在压头作用的局部区域内;同时,根据最小势能原理建立了泡沫铝夹芯板在半球形压头作用下的压入力学响应理论预测模型。通过引入无量纲参数分析了夹芯板压入载荷-位移响应,并在不同面板厚度、芯层厚度和芯层相对密度情况下,对夹芯板压入响应理论解的有效性和适用性进行了讨论。
英文摘要:
      Deformation and failure characteristics of a sandwich panel structure including composite faceplate and closed cell foamed aluminum core were experimentally investigated under quasi-static indentation condition, based on material test system (MTS). Experimental results show that the failure of the sandwich panel is mainly concentrated in the local area of pressure head. At the same time, a theoritical model predicting indention mechanical response of foamed aluminum sandwich panel due to hemispherical pressure head action was established based on principle of minimum potential enenrgy. By introducing a dimensionless parameter, the relation between indentation load and indentation depth of sandwich panel was analyzed. The validity and applicability of theoretical response prediction were discussed for sandwich panels with different faceplate thicknesses, core thicknesses and core relative densities, respectively.
查看全文  下载PDF阅读器
关闭

网站版权:《实验力学》编辑部
您是本站第 65668819 位访问者,今日一共访问992次,当前在线人数: 0
技术支持:本系统由北京勤云科技发展有限公司设计