崔海涛, 温卫东, 郝 勇. 碳纤维增强复合材料含孔层合板损 伤破坏分析研究进展 [J]. 材料导报, 2002, 16(2): 43-45. Cui Haitao, Wen Weidong, Hao Yong. Advances in damage analysis for carbon fiber-reinforced composite laminates with hole [J]. Material Report, 2002, 16(2): 43-45.
[2]
程小全, 康炘蒙, 邹 健, 等. 平面编织复合材料层合板低速冲击后拉伸性能 [J]. 复合材料学报, 2008, 25(5): 163-168. Cheng Xiaoquan,Kang Xinmeng, Zou Jian, et al. Tensile properties of plane woven composite laminates after low velocity impact [J]. Acta Materiae Compositae Sinica, 2008, 25(5): 163-168.
[3]
Knight N F, Jr. Factors influencing progressive failure analysis predictions for laminated composite structure // Proceedings of the 49th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. Schaumburg, Illinois: AIAA, 2008.
[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]
Chang F K, Lessard L. Damage tolerance of laminated composites containing an open hole and subjected to tensile loadings [J]. Journal of Composite Materials, 1991, 25(3): 274-301.
[6]
Tan S. A progressive failure model for composite laminates containing openings [J]. Journal of Composite Materials, 1991, 25(6): 556-574.
[7]
Gama B A, Xiao J R, Haque M J, et al. Experimental and numerical investigations on damage and delamination in thick plain weave S-2 glass composites under quasi-static punch shear loading // 18th Annual Technical Conference of American Society for Composites. Gainesville, Florida: University of Florida, 2003.
[8]
Ambur D R, Jaunky N, Dávila C G. Progressive failure of composites laminates using LaRC02 failure criteria // Proceedings of the 45th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. Palm Springs, California: AIAA, 2004.
[9]
Camanho P P, Maimi P, Dávila C G. Prediction of size effects in notched laminates using continuum damage mechanics [J]. Composite Science and Technology, 2007, 67(13): 2715-2727.
[10]
Lapczyk I, Hurtado J A. Progressive damage modeling in fiber-reinforced materials [J]. Composites Part A, 2007, 38(11): 2333-2341.
[11]
Lorriott T, Marion G, Harry R, et al. Onset of free-edge delamination in composite laminates under tensile loading [J]. Composites Part B, 2003, 34(5): 459-471.
[12]
Yang Q, Cox B. Cohesive models for damage evolution in laminated composites [J]. International Journal of Fracture,133(2): 107-137.
[13]
Hashin Z, Rotem A. A fatigue failure criterion for fiber-reinforced composite materials [J]. Journal of Composite Materials, 1973, 7(5): 448-464.
[14]
ABAQUSrM user's manual, Vol 1-3 [M]. Version 6.10. Pawtucket, Rhode Island: Hibbitt, Karlsson, and Sorensen, 2010.
[15]
Turon A, Dávila C G, Camanho P P, et al. An engineering solution for mesh size effects in the simulation of delamination using cohesive zone models [J]. Engineering Fracture Mechanics, 2007, 74(10): 1665-1682.
[16]
Hallett Stephen R, Jiang Wenguang, Wisnom Michael R. The effect of stacking sequence on thickness scaling of tests on open hole tensile composite specimens // 48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. Honolulu, Hawaii: AIAA, 2007.