Dynamic Detection Method of Delamination Damage for Composite Laminates
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摘要: 针对复合材料层合板在加工、服役过程中经常发生分层损伤的问题,提出了基于曲率模态参数的损伤评价方法。运用有限元理论对层合板不同损伤状态下的振动特性进行数值模拟;再基于计算所得参数,运用中心差分法分别计算其均布载荷的曲面值曲率和振型曲率;最后将此曲率参数与未损伤模型参数作差分以辨别损伤。数值计算结果表明,运用均布载荷的曲面值曲率和振型曲率均可有效识别损伤位置和损伤数量,且损伤所处层的位置会影响损伤识别指标的大小。Abstract: In this paper, a method of damage evaluation based on curvature modal parameters was proposed to detect delamination defects of the composite laminates caused during the processing or service process. Firstly, based on the finite element method, the vibration behavior of the composite laminates was simulated for delamination damages of different locations and damage degree. Then, the central difference method was used to calculate the uniform load surface (ULS) curvature and mode curvature respectively. Based on the curvature parameter, the delamination defect can be identified by using difference method. Number of numerical results show that the delamination defects can be detected effectively in the composite laminate from vibration signals by using the ULS curvature and mode curvature, and the size of damage identification index will be affected by the location of damage in different layers.
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[1] 喻溅鉴,周储伟. 复合材料疲劳分层的界面单元模型[J]. 复合材料学报, 2009, 26(6):167-172. [2] XIE D,BIGGERS S B. Progressive crack growth analysis using interface element based on the virtual crack closure technique[J]. Finite Element in Analysis and Design, 2006, 42:977-984.
[3] 孙先念,陈浩然,苏长键,等.含分层损伤复合材料层压板分层扩展研究[J].力学学报,2000,32(2):223-232. [4] 沈真.含缺陷复合材料层合板的压缩破坏机理[J]. 航空学报, 1991, 12(3):105-113. [5] 白瑞祥,陈浩然.含分层损伤复合材料加筋层合板的分层扩展研究[J].应用数学和力学,2004(4):368-378. [6] 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, 25(1):140-146. [7] ZHANG Z, AKTAN A E. Appliacation of modal flexibility and its derivatives in structural identication[J]. Resnondestr Eval, 1998, 10:43-61.
[8] PANDEY A K, BISWAS M, SAMMAN M M. Damage detection from changes in curvature mode shapes[J]. Journal of Sound and Vibration, 1991, 145(2):321-332.
[9] ZHAO Shiyang,XUE Pu. New two-dimensional polynomial failure criteria for composite materials[J]. Advances in Materials Science and Engineering, 2014, 3:1-7.
[10] 赵士洋,薛璞. 损伤变量对复合材料损伤演化过程的影响分析[J]. 西北工业大学学报, 2014, 32(4):542-545. [11] TIAN Shuxia, CHEN Zhenmao, CHEN Lingli, et al.Numerical analyses on influence of damage configuration on vibration parameters for lattice sandwich plate[J].International Journal of Applied Electromagnetics and Mechanics,2010,33(3/4):1565-1572.
[12] 田淑侠,陈振茂,樊江磊, 等. 基于动态响应参数的点阵桁架夹芯板脱焊损伤检测数值方法研究[J].应用力学学报, 2016,33(5):786-791. [13] 焦敬品,郑磊,池永斌,等.基于随机振动响应谐振频率偏移的绝缘子无损检测方法[J].无损检测,2012,34(8):17-21.
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