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综述了含损伤复合材料层合板剩余压缩强度的研究进展,重点介绍受低速冲击后复合材料层合板的剩余压缩强度问题,主要包括:(1)层合板压缩失效的损伤特征及损伤状态表征;(2)层合板压缩试验研究;(3)损伤模型分析及失效分析;(4)研究展望.

参考文献

[1] 杨光松.损伤力学与复合材料损伤[M].北京:国防工业出版社,1995
[2] 唐啸东,杨旭,陈业标.带损伤复合材料层压板剩余强度估算方法研究[J].航空学报,1997(02):146.
[3] Richardson M O W;Wisheart M J .Review of low velocity impact properties of composite materials[J].Composites Part A:Applied Science and Manufacturing,1996,27(12):1123-1131.
[4] M.F.S.F. de Moura;A.T. Marques .Prediction of low velocity impact damage in carbon-epoxy laminates[J].Composites, Part A. Applied science and manufacturing,2002(3):361-368.
[5] Elder D J;Thomsonb R S et al.Review of delamination predictive methods for low speed impact of composite laminates[J].Computers and Structures,2004,66(04):677-683.
[6] 沈真,张子龙,王进,杨胜春,叶林.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(05):140-145.
[7] Dost E F;Avery W B;Finn L B.Impact damage resistance of composite fuselarge structure,part 3[A].,1993
[8] Lee S M;Zahuta P .Instrumented impact and static indentation of composites[J].Journal of Composite Materials,1991,25(02):204-222.
[9] ASTM D 7137-05.Standard test method for compressive residual strength properties of damaged polymer matrix composite plates[S].,2005.
[10] 杨旭,沈真,燕瑛,刘兵山.复合材料韧性评定的新方法关于损伤阻抗性能的研究[J].中国航空学报(英文版),2003(02):73-79.
[11] 沈真,柴亚南,杨胜春,章怡宁,黎观生.复合材料飞机结构强度新规范要点评述[J].航空学报,2006(05):784-788.
[12] 沈真,杨胜春,陈普会.复合材料抗冲击性能和结构压缩设计许用值[J].航空学报,2007(03):561-566.
[13] 沈真,杨胜春,陈普会.复合材料层压板抗冲击行为及表征方法的实验研究[J].复合材料学报,2008(05):125-133.
[14] Toshio Abe;Kengo Hayashi;Fumihito Takeda.A VARTM for primary aircraft structures[A].Paris:SAMPE,2005:3792384.
[15] 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(06):8-12.
[16] 程小全,寇长河,郦正能.低速冲击后复合材料层合板的压缩破坏行为[J].复合材料学报,2001(01):115-119.
[17] 崔海坡,温卫东.T300/BMP316层合板冲击后压缩强度试验[J].航空动力学报,2008(11):2001-2006.
[18] Nettles A T;Hedge A J.Compression-after-impact tesring of thin composite materials[A].,1991:177-183.
[19] S. Sanchez-Saez;E. Barbero;R. Zaera;C. Navarro .Compression after impact of thin composite laminates[J].Composites science and technology,2005(13):1911-1919.
[20] 张子龙,程小全,益小苏.复合材料冲击损伤及冲击后压缩强度的等效实验方法[J].实验力学,2001(03):313-319.
[21] Pavier J;Clarker M P .A specialized composite plate element for problems of delamination buckling and growth[J].Computers and Structures,1996,34(01):43-53.
[22] Paolo Gaudenzi .On delamination buckling of composite laminates under compressive loading[J].Computers and Structures,1997,39(01):21-30.
[23] 郭兆璞,陈浩然.含分层损伤复合材料层合板的压缩强度研究[J].固体力学学报,2000(02):117-122.
[24] J. Lee;C. Soutis .Thickness effect on the compressive strength of T800/924C carbon fibre-epoxy laminates[J].Composites, Part A. Applied science and manufacturing,2005(2):213-227.
[25] Lee J;Soutis C .Measuring the notched compressive strength of composite laminates:specimen size elects[J].Computer Science and Technology,2008,68(12):2359-2366.
[26] J. Lee;C. Soutis .A study on the compressive strength of thick carbon fibre-epoxy laminates[J].Composites science and technology,2007(10):2015-2026.
[27] Timeshenko S.Theory of Elasticity[M].McGraw-Hill,1951
[28] Jackson W C;Poe C C Jr.The use of impact force as a scale parameter for the impact response of composite laminates[A].,1992:981-998.
[29] 郑晓霞,郑锡涛,沈真,杨胜春.低速冲击与准静态压痕力下复合材料层合板的损伤等效性[J].航空学报,2010(05):928-933.
[30] Hosur M V;Murthy C R L;Ramurthy T S .Compression after impact testing of carbon fibre reinforced plastic laminates[J].Journal of Computer Technology and Research,1999,21:51-64.
[31] Papanicolaou G C;Sravropoulos C D .New approach for residual compressive strength prediction of impacted cfrp laminates[J].Composites,1995,26(07):517-523.
[32] 崔海坡,温卫东,崔海涛.复合材料层合板冲击损伤及剩余强度研究进展[J].材料科学与工程学报,2005(03):466-472.
[33] 林智育,许希武.复合材料层板低速冲击后剩余压缩强度[J].复合材料学报,2008(01):140-146.
[34] F. Laurin;N. Carrere;J.-F. Maire .Laminated composite structures subjected to compressive loading: A material and structural buckling analysis[J].Composite structures,2007(2):172-182.
[35] F. Laurin;N. Carrere;J.-F. Maire .A multiscale progressive failure approach for composite laminates based on thermodynamical viscoelastic and damage models[J].Composites, Part A. Applied science and manufacturing,2007(1):198-209.
[36] Maire J F;Chaboche J L .A new formulation of continuum damage mechanics(CDM)for composite materials[J].Aerospace Science and Technology,1997,1(04):247-257.
[37] 李仲,葛森,杨胜春,吕国志.含损伤缝合复合材料层压板压缩剩余强度估算方法[J].西北工业大学学报,2007(03):342-346.
[38] 崔海坡,温卫东,崔海涛.层合复合材料板的低速冲击损伤及剩余压缩强度研究[J].机械科学与技术,2006(09):1013-1017.
[39] X.W. Wang;I. Pont-Lezica;J.M. Harris .Compressive failure of composite laminates containing multiple delaminations[J].Composites science and technology,2005(2):191-200.
[40] Zuleyha Asian;Mustafa Sahin .Buckling behavior and compressive failure of composite laminates containing multiple large delaminations[J].Composite structures,2009(3):382-390.
[41] Andrew T;Rhead;Richard Butler.Compressive static strength model for impact danaged laminates[J].Computer Science and Technology,2009(69):2301-2307.
[42] 林智育,许希武.含冲击损伤复合材料加筋层板压缩剩余强度[J].航空学报,2009(01):56-61.
[43] Yeh H Y;Kim C H .The Yeh-stratton criterion for composite materials[J].Journal of Composite Materials,1994,28:926-939.
[44] 孙先念,陈浩然,苏长健,刘相斌.含分层损伤复合材料层合板剩余压缩强度研究[J].应用力学学报,2000(04):138-143.
[45] 赵美英,万小朋,张延辉.复合材料含损伤结构剩余强度分析[J].机械强度,2001(02):129-130,186.
[46] Chang Kuoyen;Liu Sheng .Damage tolerance of laminated composites containing an open hole and subjected to tensile loadings[J].Journal of Composite Materials,1991,25(03):274-301.
[47] Tan S C .A progressive failure model for composite laminates containing opening[J].Journal of Composite Materials,1991,25(05):556-577.
[48] P. P. Camanho;F. L. Matthews .A progressive damage model for mechanically fastened joints in composite laminates[J].Journal of Composite Materials,1999(24):2248-2280.
[49] B. Qi;I. Herszberg .An engineering approach for predicting residual strength of carbon/ epoxy laminates after impact and hygrothermal cycling[J].Composite Structures,1999(1/4):483-490.
[50] Chang Fukuo;Chang Kuoyen .A progressive damage model for laminated composites containing stress concentrations[J].Journal of Composite Materials,1987,21:834-855.
[51] Soutis C N;Fleck A;Smith P A .Failure prediction technique for compression loaded carbon fibre-epoxy laminate with a single hole[J].Journal of Composite Materials,1991,25(14):76-98.
[52] 关长文,陈浩然,成万植.复合材料和结构机械连接件破坏历程的数值模拟与试验验证[J].航空学报,1995(02):143.
[53] Whitney J M;Nuismer R J .Stress fracture criteria for laminates containing concentrations[J].Journal of Composite Materials,1974,8:253-275.
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