对T300/BMP-316单向层合板静载及疲劳加载各主方向损伤失效进行了试验研究,为建立该材料各主方向疲劳加载剩余刚度退化表达式及剩余强度退化表达式提供了依据.同时,获得了该材料剪切非线性因子,给出了面内剪切疲劳加载试验循环过程中剪切刚度计算公式,使用渗透剂增强的X射线图像技术对试样静载及疲劳破坏损伤状态进行了无损检测,并对损伤失效机理形式进行了分析探讨.试验表明,层合板结构应力分析中考虑材料剪切应力-应变的非线性效应是非常必要的.
参考文献
| [1] | 王丹勇.层合板接头损伤失效与疲劳寿命研究[D].南京:南京航空航天大学,2006:34-60. |
| [2] | 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.Three-dimensional progressive damage analysis of single fastener joints in composite laminates[J].Acta Materiae Compositae Sinica,2005,22(3):168-174. |
| [3] | 王丹勇,温卫东,崔海涛.含孔复合材料层合板静拉伸三维逐渐损伤分析[J].力学学报,2005,37(6):788-795.Wang Danyong,Wen Weidong,Cui Haitao.Three-dimensional progressive damage analysis of composite laminates containing a hole subjected to tensile loading[J].Chinese Journal of Theoretical and Applied Mechanics,2005,37(6):788-795. |
| [4] | 王丹勇,温卫东,崔海涛.含材料非线性的复合材料单钉接头累积损伤分析[J].固体力学学报,2006,27(2):186-190.Wang Danyong,Wen Weidong,Cui Haitao.Progressive damage analysis considering the material nonlinearity of composite laminates containing a hole[J].Acta Mechanica Solida Sinica,2006,27(2):186-190. |
| [5] | 罗祖道,王震鸣.复合材料力学进展[M].北京:北京大学出版社,1992:62-65. |
| [6] | Shokrich M M,Lessard L B.Multiaxial fatigue behaviour of unidirectional plies based on uniaxial fatigue experiments Ⅱ:Experimental evaluation[J].International Journal of Fatigue,1997,19(3):209-217. |
| [7] | Kilic H.Progressive damage and nonlinear analysis of pultruded composite structures[J].Composites Part B,2003,34(3):235-250. |
| [8] | Hahn H T,Tsai S W.Nonlinear elastic behavior of unidirectional composite laminae[J].Journal of Composite Materials,1973,7(1):102-118. |
| [9] | Hassani F,Shokreh M,Lessard L.A fully non-linear 3-D constitutive relationship for the stress analysis of a pin-loaded composite laminate[J].Composites Science and Technology,2002,62(3):429-439. |
| [10] | Nahas M N.Analysis of non-linear stress-strain response of laminated fibre-reinforced composites[J].Fibre Science and Technology,1984,20(4):297-313. |
| [11] | Shokrieh M M,Lessard L B.Effects of material nonlinearity on the three-dimensional stress state of pin-loaded composite laminates[J].Journal of Composite Materials,1996,30(7):839-861. |
| [12] | 沈观林.复合材料力学[M].北京:清华大学出版社,1996:134-136. |
| [13] | 国家技术监督局.GB/T 16779-1997纤维增强塑料层合板拉-拉疲劳性能试验方法[S].北京:中国标准出版社,1997:1-6. |
| [14] | 国家技术监督局.GB/T 3354-1999定向纤维增强塑料拉伸性能试验方法[S].北京:中国标准出版社,1999:1-7. |
| [15] | 国家技术监督局.GB/T 5258-1995纤维增强塑料薄层板压缩性能试验方法[S].北京:中国标准出版社,1995:1-8. |
| [16] | 航空工业总公司.GJB 2637-1996碳纤维树脂基复合材料层合板疲劳试验方法[S].北京:国防科工委军标出版社,1996:1-8. |
| [17] | 赵渠林.先进复合材料手册[M].北京:机械工业出版社,2003:1766-1767. |
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