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建立了有效的复合材料层合板结构冲击损伤分析方法,层合板面内损伤采用改进的Chang/Chang失效准则做判据,得到面内各类损伤形式.层间损伤采用与Mixed-Mode粘接元等效的TIEBREAK接触模拟.利用此分析方法,从复合材料薄壁结构设计需要出发,研究了在低能量冲击下,铺层的层间角度、铺层方向、铺层重叠对层合板结构冲击损伤阻抗的影响规律,并对它们的综合影响进行了总体分析,得到了能提高层合板结构损伤阻抗的铺层顺序设计指导.最后用该设计指导对某种铺层结构进行了重新设计和有限元模拟,验证了该设计指导的可行性和有效性.

参考文献

[1] 沈真,刘峰.新的韧性复合材料评定技术623S-200101-114[R].西安:中国飞机强度研究所,2001.Shen Zhen,Liu Feng.New toughness composite evaluation technology.623S-200101-114[R].Xi'an:Aircraft Strength Institute of China,2001.
[2] Collombet F,Lalbin X,Bonini J,et al.Damage criteria for the study of impacted composite laminates[J].Composites Science and Technology,1998,58(5):679-686.
[3] Choi H Y,Wang H S,Chang F K.Effect of laminate configuration and impactor's mass on the initial impact damage of graphite/epoxy composite plates due to line-loading impact[J].Journal of Composite Materials,1992,26(6):804-827.
[4] Chang F K,Chang K Y.A progressive damage model for laminated composites containing stress concentrations[J].Journal of Composite Materials,1987,21(9):834-855.
[5] Hou J P,Petrinic N,Ruiz C,et al.Prediction of impact damage in composite plates[J].Composites Science and Technology,2000,60(2):273-281.
[6] Caprino G.Residual strength prediction of impacted CFRP laminates[J].Journal of Composite Materials,1984,18(6):508-518.
[7] Camanho P P,Dávila C G.Mixed-mode decohesion finite elements for the simulation of delamination in composite materials[J].NASA-Technical Paper,2002,211737 (1):33.
[8] Hallquist J O.LS-DYNA keyword user's manual[M].Volume Ⅰ and Ⅱ,Version 971 R6.0.0.California:Livermore Software Technology Corporation,2012:246-249.
[9] Camanho P P,Davila C G,de Moura M F.Numerical simulation of mixed-mode progressive delamination in composite materials[J].Journal of Composite Materials,2003,37(16):1415-1438.
[10] Benzeggagh M L,Kenane M.Measurement of mixed-mode delamination fracture toughness of unidirectional glass/epoxy composites with mixed-mode bending apparatus[J].Composites Science and Technology,1996,56(4):439-449.
[11] 温卫东,崔海坡,徐颖.T300/BMP-316复合材料板冲击损伤研究[J].航空动力学报,2007,22(5):749-754.Wen Weidong,Cui Haipo,Xu Yin.Research on impact damage of T300/BMP-316 composite laminates[J].Journal of Aerospace Power,2007,22(5):749-754.
[12] Prandy J,Boyd J,Recker H,et al.The effect of absorbed energy on the CAI performance for composite materials[C]//Proceedings of 36th International SAMPE Symposium and Exhibition,1991,36:901-911.
[13] Fuoss E,Straznicky P V,Poon C.Effects of stacking sequence on the impact resistance in composite laminates:Part 1-Parametric study[J].Composite Structures,1998,41(1):67-77.
[14] Hitchen S A,Kemp R M J.The effect of stacking sequence on impact damage in a carbon fibre/epoxy composite[J].Composites,1995,26(3):207-214.
[15] González E V,Maimí P,Camanho P P,et al.Effects of ply clustering in laminated composite plates under low-velocity impact loading[J].Composites Science and Technology,2011,71(6):805-817.
[16] 沈真,张子龙,王进,等.复合材料损伤阻抗和损伤容限的性能表征[J].复合材料学报,2004,21(5):140-145.Shen Zhen,Zhang Zhilong,Wan Jin,et al.Characterization of damage resistance and damage tolerance behaviour of composite laminates[J].Acta Materiae Compositae Sinica,2004,21(5):140-145.
[17] 程小全,张子龙,吴学仁.小尺寸试件层合板低速冲击后的剩余压缩强度[J].复合材料学报,2002,19(6):8-12.Cheng Xiaoquan,Zhang Zilong,Wu Xueren.Post-impact compressive strength of small composite laminate specimens[J].Acta Materiae Compositae Sinica,2002,19(6):8-12.
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