期刊文献+

含孔隙碳纤维/环氧树脂层合板力学性能模拟 被引量:10

Simulation on mechanical properties of carbon fiber reinforced epoxy laminates with voids
下载PDF
导出
摘要 为了探究孔隙率对织物碳纤维/环氧树脂复合材料层合板拉伸强度和压缩强度的影响规律,分别测量了孔隙率为0.33%、0.71%及1.50%的复合材料层合板的拉伸强度及压缩强度并进行有限元模拟.试验结果表明:随着孔隙率的增加,复合材料层合板的拉伸强度和压缩强度均呈下降趋势.建立了适用于织物纤维增强复合材料的静态力学强度的失效准则,结合刚度突然退化模型,通过引入不同孔隙率复合材料的基本强度参数,使用ABAQUS软件建立有限元模型,对不同孔隙率的织物碳纤维/环氧树脂复合材料层合板的拉伸强度及压缩强度进行了较为准确的预测. The study investigated the influence of the porosity on the tensile strength and compressive strength of the carbon fiber fabric reinforced epoxy composites laminates.The tensile strength and compressive strength test on the carbon fiber reinforced polymer(CFRP) laminates with porosity of 0.33%,0.71% and 1.50% were conducted and simulated by a finite element analysis model.The experiment results show that the tensile strength and compressive strength decrease as the void contents increase.The failure criterion of static mechanical strength of the fabric fiber reinforced composites is provided.Basic strength parameters of composites were used to evaluate the mechanical properties of CFRP laminates with different porosities.A finite element analysis model was established by using ABAQUS software,combined with a model of sudden stiffness degradation.The tensile strength and compressive strength of the fabric carbon fiber reinforced the epoxy composites laminates were accurately simulated.
出处 《哈尔滨工程大学学报》 EI CAS CSCD 北大核心 2013年第3期389-393,共5页 Journal of Harbin Engineering University
关键词 复合材料层合板 碳纤维 孔隙 有限元模拟 强度预测 composites laminates carbon fiber void finite element simulation strength prediction
  • 相关文献

参考文献9

  • 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. 被引量:1025
  • 2ATADERO R A, KARBHARI V M. Calibration of resistance factors for reliability based design of externally-bonded FRP composites[J]. Composites: Part B, 2008, 39(4): 665-679.
  • 3MAROUANI S, CURTIL L, HAMELIN P. Composites realized by hand lay-up process in a civil engineering environment: initial properties and durability [ J ]. Materials and Structures, 2008, 41(5): 831-851.
  • 4BIRT E A, SMITH R A. A review of NDE methods for porosity measurement in fibre-reinforced polymer composites [ J ]. Non-Destructive Testing and Condition Monitoring, 2004, 46 ( 11 ) : 681-686.
  • 5PARK S Y, CHOI W J, CHOI H S. The effects of void contents on the long-term hygrothermal behaviors of glass/ epoxy and GLARE laminates[J]. Composite Structures, 2010, 92(1) : 18-24.
  • 6COSTA M L, ALMEIDA S F M, REZENDE M C. The influence of porosity on the interlaminar shear strength of carbon epoxy and carbon bismaleimide fabric laminates [ J ]. Composites Science and Technology, 2001, 61 (14) : 2101-2108.
  • 7CHAMBERS A R, EARL J S, SQUIRES C A, et al. The effect of voids on the flexural fatigue performance of unidirectional carbon fiber composites developed for wind turbine applications[ J]. International Journal of Fatigue, 2006, 28 (10) : 1389-1398.
  • 8ALMEIDA S F M, NETO Z S N. Effects of void content on the strength of composite laminates [ J ]. Composite Structure, 1994, 28(2): 139-148.
  • 9SHOKRIEH M M, LESSARD L B. Progressive fatigue damage modeling of composite material, part I: modeling [J]. Journal of Composite Materials, 2000, 34 (13): 1056-1080.

二级参考文献35

  • 1陈绍杰.复合材料与B7E7"梦想"飞机[J].航空制造技术,2005,48(1):34-37. 被引量:22
  • 2张卫红,吴琼,高彤.周期性金属桁架夹芯板的力学性能研究进展[J].昆明理工大学学报(理工版),2005,30(6):24-28. 被引量:7
  • 3章继峰,张博明,杜善义.平板型复合材料格栅结构的增强改进与参数设计[J].复合材料学报,2006,23(3):153-157. 被引量:13
  • 4师昌绪.材料大词典[M].北京:化学工业出版社,1994..
  • 5EDAS Deutschland GmbH, Corporate Research Center. The research requirements of the transport sectors to facilitate an increased usage of composite materials I: The composite material research requirements of the aerospace industry [EB/OL]. [2006- 12- 27] http:// gcep. stanford, edu/pdfs/as-sessment s/adv_t ransportation_assessment, pdf.
  • 6Darrel T, Byron R P. Advanced composites development for aerospace applications [EB/OL]. [2006-12-27]. http://cite-seer. ist. psu. edu/cache/papers/cs/29702/ftp: zSzzSztechreports, larc. nasa. govzSzpubzSztlzSzmtgzS zNASA-2001 - 7sampe- drt. pdf/advanced - composites - developme nt- for. pdf.
  • 7Rehfield W R, Cheung R H. SOme basic strategies for aeroelastic tailoring o{ wings with bend-twist coupling [C] //44^th AIAA/ASME/ASCE/AHS Structures, Structural Dynamics and Materials Conference. Norfolk, Virginia: American Institute of Aeronautics and Astronautics, lnc, 2003 : 7-10.
  • 8National Aerospace Laboratory NLR. Aerospace structures and materials status report 2003 [EB/OL]. www. nrel. gov/ncpv/t hin_film/docs/world_pv_st at us_rpt_2003, pdf.
  • 9Robinson M J. A qualitative analysis of some of the issues affecting the cost of composites structures [C]// Proc. 23^th International SAMPE Technical Conf. Covina CA: Society for the Advancement of Material and Process Engineering, 1991: 445-458.
  • 10Steven H. Analysis and behavior of grid structures [D]. Stanford: Stanford University, 1995.

共引文献1024

同被引文献45

引证文献10

二级引证文献55

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部