X-cor夹层结构的剪切性能

单杭英; 肖军; 尚伟; 李宁; 张向阳

X-cor夹层结构的剪切性能

单杭英^1,2,
肖军¹,
尚伟¹,
李宁¹,
张向阳¹

1.
南京航空航天大学材料科学与技术学院,南京 210016
2.
南京航空航天大学无人机研究院,南京 210016

基金项目: 科研项目(JPPT-1146)

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出版历程
- 收稿日期: 2012-07-09
- 刊出日期: 2013-03-28

Shear properties of X-cor sandwich

1.
College of Material Science and Technology, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
2.
Research Institute of Unmanned Aircraft, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China

摘要

摘要: 通过X-cor夹层结构与相同材料同尺寸的未增强件和去除泡沫的Z-pin夹层结构进行剪切性能试验对比,考察Z-pin对泡沫夹层结构的增强效果.通过剪切刚度和剪切强度试验值和理论值的对比分析研究,得到了修正后的夹层结构剪切刚度和剪切强度理论计算公式.研究结果表明:夹层结构的剪切性能与剪切刚度折减系数M、表征加载过程中Z-pin开始从面板拔出的时间系数T有关,而系数M,T决定于工艺水平.
- X-cor夹层结构 /
- 剪切性能 /
- 刚度折减 /
- 时间系数T /
- 工艺水平
Abstract: A series of experiments were carried out for comparison under shear loading,including X-cor sandwich,foam sandwich and Z-pin sandwich,so as to investigate Z-pin enhancement effect on foam sandwich.By studying on the difference between test and formual data the modifed formula of shear modulus and strength was achieved.The result shows that shear properties are related to modulus stiffness discount M and time facotr T,indicating the beginning of Z-pin pull from face skin: M and T were affirmed by craft level.
- X-cor sandwich /
- shear properties /
- stiffness discount /
- time facotr T /
- craft level

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参考文献(19)

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