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综述了碳纤维增强复合材料含孔层合板损伤破坏以及应力分析的研究进展,介绍了几种含孔层合板的破坏准则和分析含孔层合板损伤破坏的二维以及三维模型,展望了有待于进一步研究的问题.

参考文献

[1] 方岱宁.先进复合材料的宏微观力学与强韧化设计:挑战与发展[J].复合材料学报,2000(02):1-7.
[2] Shahid I.;Chang FK. .AN ACCUMULATIVE DAMAGE MODEL FOR TENSILE AND SHEAR FAILURES OF LAMINATED COMPOSITE PLATES[J].Journal of Composite Materials,1995(7):926-981.
[3] Chang F K;Larry B L .Damage tolerance of laminated composites containing an open hole and subjected to compressive loadings:Part I-Analysis[J].Journal of Composite Materials,1991,25:2.
[4] Grews J H .A survey of strength analysis methods for laminates with holes[J].Journal of aeronautical society of INDIA,1984,36:287.
[5] Chang K Y;Liu S;Chang F K .Damage tolerance of lami nated composites containing an open hole and subjected to tensile loadings[J].Journal of Composite Materials,1991,25:274.
[6] Tan S C .A progressive failure model for composite lami nates containing openings[J].Journal of Composite Materials,1991,25:556.
[7] Alan R. Kallmeyer;Ralph I. Stephens .A finite element model for predicting time-dependent deformations and damage accumulation in laminated composite bolted joints[J].Journal of Composite Materials,1999(9):794-826.
[8] Reifsmider K;Case S;Duthoit J .The mechauics of com posite strength evolution[J].Journal of Computer Science and Technology,2000,60:2539.
[9] 胡伟平,孟庆春,张行.含内部分层复合材料层板三维问题的三角级数能量解法[J].复合材料学报,1998(03):113-118.
[10] Kashtalyan M;Soutis C .The effect of delaminations in duced by transverse cracks and splits on stiffness proper ties of composite laminates[J].Composites Part A:Applied Science and Manufacturing,2000,31:107.
[11] Gamble K;Pilling M;Wilson A .An automated finite element analysis of the initiation and growth of damage in carbon-fiber composite materials[J].Computers and Structures,1995,135:265.
[12] P. P. Camanho;F. L. Matthews .Delamination onset prediction in mechanically fastened joints in composite laminates[J].Journal of Composite Materials,1999(10):906-927.
[13] Camanho P P;Matthews F L .A progressive damage model for mechancally fastened joints in composite laminates[J].Journal of Composite Materials,1999,33(24):2248.
[14] Wilt T E;Murthy P L N;Chamis C C.Fracture tough ness computational simulation of general delaminations in fibre composites[A].Virginia:Williamburg,1988:355.
[15] Nguyen B N .Damage modeling of laminated composites by the use of multilayer volume elements[J].Journal of Computer Science and Technology,1998,58:891.
[16] Wei-Hwang Lin;Ming-Hwa R. Jen .The strength of bolted and bonded single-lapped composite joints in tension[J].Journal of Composite Materials,1999(7):640-666.
[17] Morais A. B.; .Open-hole tensile strength of quasi-isotropic laminates[J].Composites science and technology,2000(10):1997-2004.
[18] Gong X L;Gong X J .Application of Tsai-Wu criterion to notched and unnothced composite laminates under torque loading[J].Journal of Composite Materials,2000,34(06):460.
[19] 赵时熙;王波;陈焕春.高模量碳环氧复合材料混合模式分层断裂研究[J].中国空间科学技术,1998(05):25.
[20] 孙先念,陈浩然,陈绍杰.含椭圆分层损伤复合材料层合板分层前缘接触效应研究[J].复合材料学报,2000(04):105.
[21] Iarve EV. .SPLINE VARIATIONAL THREE DIMENSIONAL STRESS ANALYSIS OF LAMINATED COMPOSITE PLATES WITH OPEN HOLES[J].International Journal of Solids and Structures,1996(14):2095-2118.
[22] Endel I .Three-dimensional stress analysis in laminated composites with fasteners based on the B-Spline approximation[J].Composites Part A:Applied Science and Manufacturing,1997,28:559.
[23] Mollenhauer DH.;Rose DH.;Schaff JR. .Experimental verification of spline stress analysis method for a structural composite laminate containing a hole[J].Journal of Reinforced Plastics and Composites,1998(2):96-108.
[24] 郭玉翠,范天佑.纤维增强复合材料断裂的宏微观结合模型[J].复合材料学报,1999(01):137-141.
[25] 傅志平;曹志远 .复合材料构件性能的细观元分析[J].复合材料学报,1998,15(01):108.
[26] Zhang J Q;Herrmann K P .Stiffness degradation induced by multilayer intralaminar cracking in composite laminates[J].Composites Part A:Applied Science and Manufacturing,1999,30:683.
[27] Hu N.;Wang B. .Effective elastic properties of 2-D solids with circular holes: numerical simulations[J].Composites science and technology,2000(9):1811-1823.
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