Meo M, Morris A J, Vignjevic R, et al. Numerical simulations of low-velocity impact on an aircraft sandwich panel[J]. Composite Structures, 2003, 62(3): 353-360.
[2]
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.
[3]
Aymerich F, Dore F, Priolo P. Prediction of impact-induced delamination in cross-ply composite laminates using cohesive interface elements[J]. Composites Science and Technology, 2008, 68(12): 2383-2390.
[4]
Zou Z, Reid S R, Li S, et al. Application of a delamination model to laminated composite structures[J]. Composite Structures, 2002, 56(4): 375-389.
Donadon M V, Iannucci L, Falzon B G, et al. A progressive failure model for composite laminates subjected to low velocity impact damage[J]. Computers & Structures, 2008, 86(11): 1232-1252.
[7]
毛春见, 许希武, 田静, 等. 缝合复合材料层板低速冲击损伤研究[J]. 固体力学学报, 2011, 32(1): 43-56. Mao Chunjian, Xu Xiwu, Tian Jing, et al. Studies on low-velocity impact damage of stitched composite laminates[J]. Chinese Journal of Solid Mechanics, 2011, 32(1): 43-56.
[8]
Systèmes D. Abaqus analysis user's manual[Z]. 2010.
[9]
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 Zilong, Wang Jin, et al. Characterization of damage resistance and damage tolerance behavior of composite laminates[J]. Acta Materiae Compositae Sinica, 2004, 21(5): 140-145.
[10]
Pinho S T, Dàvila C G, Camanho P P, et al. Failure models and criteria for FRP under in-plane or three-dimensional stress states including shear non-linearity, NASA/TM-2005-213530[R]. Hanpton, VA: NASA Langley Research Center, 2005.
[11]
Hashin Z, Rotem A. A fatigue failure criterion for fiber reinforced materials[J]. Journal of Composite Materials, 1973, 7(4): 448-464.
[12]
Hashin Z. Fatigue failure criteria for unidirectional fiber composites[R]. Pennsylvania: Philadelphia Department of Materials Science and Engineering, Pennsylvanina State Vinversity, 1980.
[13]
Lapczyk I, Hurtado J A. Progressive damage modeling in fiber-reinforced materials[J]. Composites Part A: Applied Science and Manufacturing, 2007, 38(11): 2333-2341.
[14]
Matzenmiller A, Lubliner J, Taylor R L. A constitutive model for anisotropic damage in fiber-composites[J]. Mechanics of Materials, 1995, 20(2): 125-152.
[15]
Wang Y, Tong M, Zhu S. Three dimensional continuum damage mechanics model of progressive failure analysis in fibre-reinforced composite laminates[C]//50th AIAA Structures, Structural Dynamics, and Materials Conference. California: American Institute of Aeronautics and Astronautics, 2009.
[16]
Li C F, Hu N, Yin Y J, et al. Low-velocity impact-induced damage of continuous fiber-reinforced composite laminates. Part I. An FEM numerical model[J]. Composites Part A: Applied Science and Manufacturing, 2002, 33(8): 1055-1062.
[17]
Camanho P P. Advances in the simulation of damage and fracture of composite structures[C]//X Reunion de Usuarios de Abaqus. Pamplona, 2005.
[18]
Xiao J R, Gama B A, Gillespie Jr J W. Progressive damage and delamination in plain weave S-2 glass/SC-15 composites under quasi-static punch-shear loading[J]. Composite Structures, 2007, 78(2): 182-196.
[19]
CYCTC Engineered Materials Inc. Mechanical properties of CYCOM？977-2-35%-12KHTS-134[M]. Arizona United States: Cytec Engineered Materials Inc, 2010.
[20]
Systèmes D. Analysis of composite materials with Abaqus[R/OL].[2013-09-03]. http://ishare.iask.sina.com.cn/f/17040149.html.
[21]
American Society for Testing and Material. D7136/D7136M-05 Standard test method for measuring the damage resistance of a fiber-reinforced polymer matrix composite to a drop-weight impact event[S]. West Conshohocken (PA): ASTM International, 2005.
[22]
Systèmes D. Abaqus user subroutines reference manual[Z]. 2010.
