| 复合材料损伤阻抗和损伤容限的性能表征 |
| |
| 引用本文： | 沈真,张子龙,王进,杨胜春,叶林.复合材料损伤阻抗和损伤容限的性能表征[J].复合材料学报,2004,21(5):140-145. |
| |
| 作者姓名： | 沈真 张子龙 王进 杨胜春 叶林 |
| |
| 作者单位： | 1.中国飞机强度研究所, 西安 710065; |
| |
| 基金项目： | 国防重点实验室基金 ( 0 0JS49.3 .1.HK5 3 0 1)资助项目，航空科学基金 ( 0 1B2 3 0 0 1)资助项目 |
| |
| 摘 要： | 复合材料结构的设计要求和使用经验提出了复合材料体系损伤阻抗和损伤容限性能表征的需求。在试验研究的基础上,本文作者指出长期以来一直使用的CAI (冲击后压缩强度) 的物理意义比较含混,有时可能误导材料研究和设计选材,同时提出应分别用典型层压板静压痕力-凹坑深度曲线的最大压痕力Fmax来表征损伤阻抗性能,用凹坑深度-压缩破坏应变曲线门槛值CAIT(Compression failure strain After Impact Threshold)来表征损伤容限性能,同时给出了测试方法的建议。
|
| 关 键 词： | 复合材料 性能表征 损伤容限 损伤阻抗 Fmax CAIT |
| 文章编号： | 1000-3851(2004)05-0140-06 |
| 收稿时间： | 2003-07-07 |
| 修稿时间： | 2003-10-30 |
CHARACTERIZATION OF DAMAGE RESISTANCE AND DAMAGE TOLERANCE BEHAVIOUR OF COMPOSITE LAMINATES |
| |
| SHEN Zhen,ZHANG Zilong,WANG Jin,YANG Shengchun,YE Lin.CHARACTERIZATION OF DAMAGE RESISTANCE AND DAMAGE TOLERANCE BEHAVIOUR OF COMPOSITE LAMINATES[J].Acta Materiae Compositae Sinica,2004,21(5):140-145. |
| |
| Authors: | SHEN Zhen ZHANG Zilong WANG Jin YANG Shengchun YE Lin |
| |
| Affiliation: | 1.Aircraft Strength Research Institute of China,Xi'an 710065, China;2.Beijing Institute of Aeronautical Materials,Beijing 100095, China;3.Shenyang Aircraft Design Research Institute, Shenyang 110035,China;4.Centre for Advanced Materials Technology, School of Aerospace, Mechanical &|Mechatronic Engineering. The University of Sydney, Sydney, NSW 2006, Australia |
| |
| Abstract: | The need to characterize damage resistance and damage tolerance behaviour of composite laminates was proposed by the design requirements and usage experience. Based on the experimental study, the authors pointed out that traditional CAI (by NASA standard) could not guide development of materials and structural design correctly. In the paper, it was proposed that the damage resistance behaviour could be characterized by the maximum contact force F_(max) of the contact force-dent depth curve of typical laminates and the damage tolerance behaviour could be characterized by the threshold CAIT(Compression failure strain After Impact Threshold) of the dent depth -compressive failure strain curve of typical laminates. In the meanwhile the suggestion for their measurement methods was proposed as well. |
| |
| Keywords: | composite materials behaviour characterization damage resistance damage tolerance F_(max) CAIT |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ |
| 点击此处可从《复合材料学报》浏览原始摘要信息 |
|
点击此处可从《复合材料学报》下载全文 |
|
