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纤维增强复合材料有效性能分散性
引用本文:宋迎东,孙志刚,高希光. 纤维增强复合材料有效性能分散性[J]. 航空动力学报, 2005, 20(2): 230-235
作者姓名:宋迎东  孙志刚  高希光
作者单位:南京航空航天大学能源与动力学院,江苏南京210016
基金项目:航空科学基金资助项目(01C52017)
摘    要:利用改进算法的宏-细观统一通用单胞本构模型,采用Monte-Carlo方法研究了不同纤维形状、不同纤维排列方式以及纤维体积含量对纤维增强复合材料弹性模量、泊松比和热膨胀系数的分散性的影响。研究结果表明:复合材料有效性能的分散性小于组分的分散性。随着纤维体积比的增加,纵向有效性能的分散性加大;而横向有效性能除了椭圆形纤维的短轴方向的热膨胀系数之外,其它性能的分散性则都是下降趋势。纤维截面形状和排列方式对纵向性能的分散性几乎没有影响。方形和圆形纤维时,横向性能的分散性几乎相同,而椭圆形纤维时,则与它们有明显的差别。不同纤维排列方式下,横向性能的分散性都是不一样的。对于E11和G12,六角形和方形对角排列时其分散性较大,而矩形排列引起的分散性最小。随着纤维体积比的增加,不同排列方式下,横向热膨胀系数的分散性趋近于一致。本文得到的结论为复合材料及结构的概率设计提供了重要的参考。 

关 键 词:航空、航天推进系统   纤维增强复合材料   有效性能   分散性   本构模型
文章编号:1000-8055(2005)02-0230-06
收稿时间:2004-03-05
修稿时间:2004-03-05

Research on Discrepancy of Fiber Reinforced Composite Effective Performance
SONG Ying-dong,SUN Zhi-gang and GAO Xi-guang. Research on Discrepancy of Fiber Reinforced Composite Effective Performance[J]. Journal of Aerospace Power, 2005, 20(2): 230-235
Authors:SONG Ying-dong  SUN Zhi-gang  GAO Xi-guang
Affiliation:College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing210016,China
Abstract:Discrepancies of elastic modulus,Poisson ratios and thermal expansion coefficients of fiber reinforced composites were investigated using the constitutive model of Cell and Monte-Carlo method.The results indicate that the discrepancies of fiber reinforced composite effective performance are smaller than the ones of their elements. With the increase of the percentage of fiber volume,the discrepancies of longitudinal effective performance increase, but that of transverse effective performances decrease,except the thermal expansion coefficient in the short-axial direction.The fiber shapes and packing arrays have little effect on the discrepancies of longitudinal effective performance.Composites with hexagonal section fibers and square cross section fibers have the same discrepancies of transverse effective performance.Different fiber packing arrays give different discrepancies.The presented conclusions in this paper are very useful to probabilistic design of composites.
Keywords:aerospace propulsion system  fiber reinforced composites  effective performances  discrepancy  constitutive model  
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