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Multi-directional composite laminates: fatigue delamination propagation in mode I-a comparison

机译:多向复合层压板:模式I-A比较中的疲劳分层传播

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Double cantilever beam (DCB) specimens composed of carbon fiber reinforced polymer laminate composites were tested. Two material systems were investigated. One consisted of plies from a woven prepreg alternating with tows in the 0 circle/90 circledocumentclass[12pt]{minimal} usepackage{amsmath} usepackage{wasysym} usepackage{amsfonts} usepackage{amssymb} usepackage{amsbsy} usepackage{mathrsfs} usepackage{upgreek} setlength{oddsidemargin}{-69pt} egin{document}$$0<^>{circ }/90<^>{circ }$$end{document}-directions and the +45 circle/-45 circledocumentclass[12pt]{minimal} usepackage{amsmath} usepackage{wasysym} usepackage{amsfonts} usepackage{amssymb} usepackage{amsbsy} usepackage{mathrsfs} usepackage{upgreek} setlength{oddsidemargin}{-69pt} egin{document}$$+45<^>{circ }/-45<^>{circ }$$end{document}-directions. The second was fabricated by means of a wet-layup process with the same multi-directions as the prepreg. In addition, for the second material system, a unidirectional (UD) fabric ply was added. The delamination for this laminate was between the UD fabric and the woven ply with tows in the +45 circle/-45 circledocumentclass[12pt]{minimal} usepackage{amsmath} usepackage{wasysym} usepackage{amsfonts} usepackage{amssymb} usepackage{amsbsy} usepackage{mathrsfs} usepackage{upgreek} setlength{oddsidemargin}{-69pt} egin{document}$$+45<^>{circ }/-45<^>{circ }$$end{document}-directions. Both fracture resistance R-curve and fatigue delamination propagation tests were carried out. It is found that the initiation value of the interface energy release rate is substantially lower for the wet-layup; whereas, their steady state values are quite similar. The fatigue delamination propagation tests were performed at various cyclic R-ratios. The delamination propagation rate da/dN was calculated from the experimental data and plotted using a modified Paris equation with different functions of the mode I energy release rate. As expected, the da/dN curves depend upon the R-ratio. By using another parameter based on the Hartman-Schijve equation for metals, it is possible to obtain a master-curve for all R-ratios. It is seen that the propagation rate for the prepreg is faster than that of the wet-layup.
机译:测试了由碳纤维增强聚合物层压复合材料组成的双悬臂梁(DCB)样本。研究了两种材料系统。其中一个由从0 Circle / 90 Circle DocumentClass [12pt]中的TOOMS交替的编织预浸料的层组成{MIMIMAL} USEPACKAGE {AMSMATH} USEPACKAGE {isysym} usePackage {AMSSYMB} USEPACKAGE {AMSBSY } usepackage {mathrsfs} usepackage {supmeek} setLength { oddsideDemargin} { - 69pt} begin {document} $$ 0 <^> { urc} / 90 <^> { cirt} $$ END {Document - } - +45圈/ -45圈 documentClass [12pt] {minimal} usepackage {ammath} usepackage {keysym} usepackage {amssymb} usepackage {amsbsy} usepackage {mathrsfs} usepackage {submeek} setLength { oddsidemargin} { - 69pt} begin {document} $$ + 45 <^> { rcire} / - 45 <^> { rcir} $$ end {document} -directions 。通过具有与预浸料坯相同的多向的湿式敷模工艺来制造第二。另外,对于第二材料系统,加入单向(UD)织物层。这种层压板的分层在UD织物和编织层之间,+45圈/ -45圈 DocumentClass [12pt] {minimal} usepackage {ammath} usepackage {isysym} usepackage {amsfonts} usepackage {amssymb} usepackage {amsbsy} usepackage {mathrsfs} usepackage {supmeek} setLength { oddsidemargin} {-69pt} begin {document} $$ + 45 <^> { cirt} / - 45 <^> { circ} $$ end {document} -directions。进行骨折抗曲线和疲劳分层繁殖试验。结果发现,湿式铺设的界面能量释放速率的起始值基本上更低;鉴于它们的稳态值非常相似。疲劳分层繁殖试验以各种环状R比进行。从实验数据计算分层传播速率DA / DN,并使用具有模式I能量释放率的不同功能的修改的巴黎方程绘制。正如预期的那样,DA / DN曲线取决于R比率。通过基于金属的Hartman-Schijve方程使用另一个参数,可以获得所有R比的主曲线。可以看出,预浸料坯的传播速率比湿式叠加的传播速率更快。

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