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含脱胶缺陷复合材料L形接头拉脱强度实验研究 被引量:5

Experimental research on tensile strength of composite L-joints with debonding defects
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摘要 为考察脱胶缺陷对整体化结构在面外拉伸载荷下承载能力的影响,实验研究了脱胶形状、间距、位置和尺寸对L形接头拉脱强度的影响规律,定量评估了脱胶对L形接头拉脱强度的影响程度,提出了脱胶缺陷对L形接头拉脱强度影响的定量表征参数。结果表明,L形接头的拉脱强度对脱胶形状、脱胶间距的变化不敏感,对脱胶位置和脱胶尺寸的变化较为敏感;位于填充区所在胶接面区域的脱胶对L形接头拉脱强度影响最大;随着脱胶尺寸特别是填充区所在胶接面脱胶尺寸的增大,拉脱强度显著降低。 To investigate the influence of debondings on the bearing capacity of integral composite structures under pull-off load condition,the influence of debonding shape,debongding space,debonding location and debonding size on the tensile strength of composite L-joints was researched with a quantitative evaluation.An important characterization parameter about the influence of debonding was proposed.The results indicate that the tensile strength of L-joints shows little sensitive change for debonding shape and debonding space.But an obvious influence of debonding location and debonding size on the tensile strength of L-joints is found,especially debonding close to the stiffener core/skin interface has the most significantly influence on the tensile strength of L-joints.The tensile strength decreases with the debonding size increasing,especially with the debonding size in the stiffener core/skin interface increasing.
出处 《复合材料学报》 EI CAS CSCD 北大核心 2012年第2期186-191,共6页 Acta Materiae Compositae Sinica
关键词 复合材料 脱胶 整体化结构 L形接头 拉脱强度 composites debonding integral structures L-joints tensile strength
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  • 1陈浩然,刘远东.动荷载作用下含损伤复合材料层合板承载能力[J].复合材料学报,2004,21(3):115-119. 被引量:10
  • 2[1]Dorey G. Impact damage in composites development, consequences and prevention. Proc. of ICCM6: sixth Int. Conf. On Composite Materials & ECCM2:2nd European Conf. on Composite Materials 3,3.1 -3.26, Elsevier Applied Science, 1987.
  • 3[2]Davies G A O,Zhang X, Edlung A. Predicting damage in composite aircraft structures due to low velocity impact. Birmingham, Structures & Materials Seminar, UK:J 1994.
  • 4Wagner W, Balzani C. Simulation of delamination in stringer stiffened fiber-reinforced composite shells [J]. Computers and Structures, 2008, 86(9): 930-939.
  • 5Zou Z, Reid S R, Li S. A continuum damage model for delaminations in laminated composites[J].Mechanics and Physics of Solids, 2003, 51: 333-356.
  • 6Hashinz Z. Failure criteria for unidirectional fiber composites [J]. J Appl Mech, 1980, 47: 329-334.
  • 7Christopher T Key, Mark R Garnich, Andrew C Hansen. Progressive failure predictions for rib-stiffened panels based on multicontinuum technology [J]. Composite and Structures, 2004, 65: 357-366.
  • 8Higgins J E, Wegner P M, Barry Van West, Adrian Viisoreanu. Postbuckling test response and analysis of fiber composite grid stiffened structures, AIAA/2002-1332[R]. Colorado: AIAA, 2002.
  • 9Garg A C.Delamination--A damage mode in composite structures[J].Engineering Fracture Mechanics,1988,29(5):557-584.
  • 10Tafreshia A,Oswald T.Global buckling behaviour and local damage propagation in composite plates with embedded delaminations[J].International Journal of Pressure Vessels and Piping,2003,80(1):9-20.

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