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含矩形边缘分层缺陷层合板的压缩性能
引用本文:程小全,王进,ALI Al-Mansour,胡仁伟,关志东. 含矩形边缘分层缺陷层合板的压缩性能[J]. 复合材料学报, 2007, 24(2): 151-158
作者姓名:程小全  王进  ALI Al-Mansour  胡仁伟  关志东
作者单位:北京航空航天大学,航空科学与工程学院,北京,100083;北京航空航天大学,航空科学与工程学院,北京,100083;沈阳飞机设计研究所,沈阳,110035
摘    要:
对含矩形边缘分层缺陷层合板的压缩性能进行试验研究和理论分析, 考察了层合板厚度(含铺层形式)、 分层位置、 形状、 面积以及环境等因素对压缩强度的影响, 并采用分层扩展以及软化夹杂两种模型对含分层层合板的压缩强度进行了计算和破坏机理分析。结果表明: 厚板对边缘分层缺陷不敏感, 中等厚度和薄层合板比较敏感; 缺陷的位置和形状对层合板压缩强度有一定的影响; 湿热环境改变了含缺陷板的压缩破坏机理, 并对中等厚度板和薄板的压缩强度有明显的影响。两种模型中软化夹杂模型效果较好, 可用于工程设计计算。 

关 键 词:层合板  分层  缺陷  压缩强度
文章编号:1000-3851(2007)02-0151-08
收稿时间:2006-04-20
修稿时间:2006-04-202006-06-12

Study on compressive properties of composite laminates with edge rectangular delamination defect
CHENG Xiaoquan,WANG Jin,ALI Al-Mansour,HU Renwei,GUAN Zhidong. Study on compressive properties of composite laminates with edge rectangular delamination defect[J]. Acta Materiae Compositae Sinica, 2007, 24(2): 151-158
Authors:CHENG Xiaoquan  WANG Jin  ALI Al-Mansour  HU Renwei  GUAN Zhidong
Affiliation:1.School of Aeronautical Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100083, China;2.Shenyang Institute of Aircraft Design and Development, Shenyang 110035, China
Abstract:
Experimental studies and theoretical analysis on compressive properties of composite laminates with the edge rectangular delamination defect were carried out.The influence of laminate thickness(including stacking sequences),delamination location,shape,area and environment on the compressive strength was discussed.Both the delamination developing model and the soft inclusion model were used to estimate the compressive strength of laminates with delamination and to analyze the failure mechanism.The results show that medium thick laminates and thin laminates are sensitive to the edge delamination defect,while thick laminates are not.The defect location and shape have a certain effect on the laminate compressive strength.The hygrothermal environment not only changes the compressive mechanism of laminates with defect,but also affects the compressive strength of medium and thin laminates.The soft inclusion model is much more effective and can be used in engineering design analysis.
Keywords:laminates   delamination   defect   compressive strength
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