EDGEWISE COMPRESSION PROPERTIES FOR HONEYCOMB SANDWICH STRUCTURE WITH PLAIN WOVEN FACEPLATE

Abstract

Abstract: In order to study the edgewise compression properties for honeycomb sandwich structure with plain woven faceplate, failure modes of honeycomb sandwich structure were divided into three types: faceplate failure, honeycomb failure. And, adhesive failure, and edgewise compression damage analysis models of honeycomb sandwich structure with plain woven faceplate were established. The honeycomb sandwich structure were predicted by the model based on progressive damage analysis. The test on edgewise compression properties of honeycomb sandwich structure were conducted. By the comparative study of the prediction and experiment results, their failure strength fitted well. The results show that the damage initiation, damage progression, and final damage during the edgewise compression of honeycomb sandwich structure can be simulated accurately by the damage analysismodel established in this paper, and finally the edgewise compression failure strength can be predicted.

Key words: plain woven, honeycomb sandwich structure, progressive damage analysis, edgewise compression properties

CLC Number:

TB332

WANG Xuan, CAO Yang-li, DENG Yun-fei, YU Ji-yuan. EDGEWISE COMPRESSION PROPERTIES FOR HONEYCOMB SANDWICH STRUCTURE WITH PLAIN WOVEN FACEPLATE[J]. Fiber Reinforced Plastics/Composites, 2018, 0(8): 5-11.

References

[1] 杜善义. 先进复合材料与航空航天[J]. 复合材料学报, 2007, 24(1): 1-12.
[2] Zabihpoor M, Adibnazari S, Moslemian R, et al. Mechanisms of fatigue damage in foam core sandwich composites with unsymmetrical carbon/glass face sheets[J]. Journal of Reinforced Plastics & Composites, 2007, 26(17): 1831-1842.
[3] 郑吉良, 孙勇, 彭明军. 等腰梯形蜂窝芯玻璃钢夹芯板的面内压缩性能[J]. 复合材料学报, 2016, 33(2): 408-417.
[4] Qiu C, Guan Z, Li Z, et al. Edgewise compression behavior of honeycomb sandwich structures[C]//Proceedings of International Conference on Mechanical and Aerospace Engineering, IEEE, 2017: 85-91.
[5] Fleck N A, Sridhar I. End compression of sandwich columns[J]. Composites Part A Applied Science & Manufacturing, 2002, 33(3): 353-359.
[6] Wang A J, Mcdowell D L. In-plain stiffness and yield strength of periodic metal honeycombs[J]. Journal of Engineering Materials & Technology, 2004, 126(2): 137-156.
[7] 杨凯, 刘立武, 于开平, 等. 带有典型缺陷的金属蜂窝夹层结构的剩余强度研究[J]. 固体火箭技术, 2011, 34(5): 652-654.
[8] 泮世东. 含面芯界面脱胶蜂窝夹芯结构的破坏行为研究[D]. 哈尔滨: 哈尔滨工业大学, 2007.
[9] 王凯伦, 黎增山, 郭俊, 等. 薄蜂窝复合材料夹芯结构侧压性能研究[J]. 科学技术与工程, 2014, 14(34): 111-116.
[10] Lei H, Yao K, Wen W, et al. Experimental and numerical investigation on the crushing behavior of sandwich composite under edge-wise compression loading[J]. Composites Part B Engineering, 2016, 94: 34-44.
[11] 杨莹. 含孔织物复合材料的强度预测与优化方法研究[D]. 南京: 南京航空航天大学, 2009.
[12] 张阿樱, 张东兴. 含孔隙碳纤维/环氧树脂层合板力学性能模拟[J]. 哈尔滨工程大学学报, 2013, 34(3): 389-393.
[13] 华洲. 复合材料蜂窝夹芯板结构损伤及其修理后仿真分析[D]. 哈尔滨: 哈尔滨工业大学, 2017.
[14] 法洋洋, 陈秀华. 蜂窝夹层结构拉脱破坏的有限元分析[J]. 机械工程材料, 2012, 36(10): 86-91.
[15] 王兴业. 夹层结构复合材料设计原理及其应用[M]. 北京: 化学工业出版社,2006: 7.
[16] 刘念超. 蜂窝芯子的力学性能计算[J]. 玻璃钢/复合材料, 1993(6): 21-24.
[17] 朱涛. 含界面脱粘蜂窝夹芯结构的屈曲和损伤扩展数值研究[D]. 天津: 天津大学, 2013.
[18] Standard test method for edgewise compressive strength of sandwich constructions: ASTM C364/C364M-16[S]. American: American Society for Testing and Materials, 2016.