为有效反映复合材料层合板层间相互作用和材料损伤非线性,建立了中等尺度的三维复合材料层合板渐进损伤分析模型.非线性渐进损伤分析过程包括应力求解、材料损伤失效判据及材料性能退化方案3个方面.讨论了损伤材料性能退化方案,引入与材料损伤模式相对应的损伤变量表征材料点的损伤状态,材料的刚度矩阵按损伤变量退化.基于该模型可成功预测复合材料层合板损伤起始、扩展直至最终失效的整个过程和极限强度.经文献试验数据验证,12种不同铺层顺序层合板的计算强度与试验数据均吻合较好,表明该模型在复合材料层合板极限强度预测上的有效性.
参考文献
| [1] | 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. |
| [2] | Chang F K,Chang K Y.Post-failure analysis of bolted composite joints in tension or shear-out mode failure[J].Journal of Composite Materials,1987,21(9):809-833. |
| [3] | Chang K Y,Lessard L B.Damage tolerance of laminated composites containing an open hole and subjected to eompresaive loadings I:Analysis[J].Journal of Composite Materials,1991,25(1):2-43. |
| [4] | Tan S C.A progressive failure model for composite laminates containing openings[J].Journal of Composite Materials,1991,25(5):556-577. |
| [5] | Tan S C,Perez J.Progressive failure of laminated composites with a hole under compressive loading[J].Journal of Reinforced Plastics and Composites,1993,12(10):1043-1057. |
| [6] | Sleight D W.Progressive failure analysis methodology for laminated composite structures,NASA/TP-1999-209107[R].Washington:NASA,1999:1-25. |
| [7] | McCarthy C T,McCarthy M A,Lawlor V P.Progressive damage analysis of multi-bolt composite joints with variable bolt-hole clearances[J].Composites Part B,2005,36(4):290-305. |
| [8] | 王丹勇,温卫东,崔海涛.复合材料单钉接头三维逐渐损伤破坏分析[J].复合材料学报,2005,22(3):168-174.Wang Danyong,Wen Weidong,Cui Haitao.Threedimensional progressive damage analysis of single fastener joints in composite laminates[J].Acta Materiae Compositae Siniea,2005,22(3):168-174. |
| [9] | 张爽,王栋,郦正能,寇长河,章怡宁.复合材料层合板机械连接结构累积损伤模型和挤压性能试验研究[J].复合材料学报,2006,23(2):163-168.Zhang Shuang,Wang Dong,Li Zhengneng,Kou Changhe,Zhang Yining.Numerical calculation of damage accumulation and bearing strength experimental verification for composite single bolted joint[J].Acta Materiae Compositae Sinica,2006,23(2):163-168. |
| [10] | Apalak Z G,Apalak M K,Genc M S.Progressive damage modeling of an adhesively bonded unidirectional composite aingle-lap joint in tension at the mesoscale level[J].Journal of Thermoplastic Composite Materials,2006,19(6):671-702. |
| [11] | Hashin Z.Failure criteria for unidirectional fiber composites[J].Journal of Applied Mechanics,1980,47(2):329-335. |
| [12] | Hashin Z,Rotem A.A fatigue failure criterion for fiber reinforced materials[J].Journal of Composite Materials,1973,7(4):448-464. |
| [13] | Puck A,Schurmann H.Failure analysis of FRP laminates by means of physically based phenomenological models[J].Composite Science and Technology,1998,58(7):1045-1067. |
| [14] | Pinho S T,Davila C G,Camanho P P,et al.Failure models and criteria for FRP under in-plane or three-dimensional stresa states including shear non-linearity,NASA/TM-2005 -213530[R].Washington:NASA,2005:1-64. |
| [15] | Maimi P,Camanho P P,Mayugo J A,Davila C G.A continuum damage model for composite laminates Ⅰ:Constitutive model[J].Mechanics of Materials,2007,39(10):897-908. |
| [16] | Lapczyk I,Hurt.ado J A.Progressive damage modeling in fiberreinforced materials[J].Composites Part A:Applied Science and Manufacturing,2007,38(11):2333-2341. |
| [17] | 徐焜,许希武.三维编织复合材料渐进损伤的非线性数值分析[J].力学学报,2007,39(3):398-407.Xu Kun,Xu Xiwu.Nonlinear numerical analysis of progressive damage of 3D braided composites[J].Chinese Journal of Theoretical and Applied Mechanics,2007,39(3):398-407. |
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