Random vibration fatigue life prediction of composite laminates based on successive ply failure mode

doi:10.19936/j.cnki.2096-8000.20241128.005

Abstract

Abstract: The random vibration fatigue life of composite laminates was studied by combining experimental and simulation methods. Vibration fatigue tests were conducted on composite laminates using a vibration table, and the natural frequency of the laminates was monitored and tracked in real-time using a laser vibration meter to obtain the random vibration fatigue life of the laminates. The finite element numerical analysis model is established. Under the random excitation, the equivalent stress power spectral density function of the random vibration of the structure is obtained. Combined with the Dirlik probability density function, the fatigue life of the laminated plate in the case of single-layer failure is obtained. The failure process of the laminated plate is simulated as the process of stiffness degradation layer by layer, continuous redistribution of stress, continuous accumulation of damage, and final overall failure. The result indicates that the error between the finite element calculation life results and the vibration fatigue test results is within the allowable range of engineering. This article can provide a feasible method for further experimental research on vibration fatigue life.

Key words: random vibration, fatigue life, composite material, laminated plates, finite element analysis

CLC Number:

TB332

SHA Zixiang, JIAN Yueao, CAI Dengan, ZHOU Guangming. Random vibration fatigue life prediction of composite laminates based on successive ply failure mode[J]. COMPOSITES SCIENCE AND ENGINEERING, 2024, 0(11): 43-49.

References

[1] 杜善义. 先进复合材料与航空航天[J]. 复合材料学报, 2007, 24(1): 1-12.
[2] 代礼葵, 孙耀宁, 王国建. 玻璃纤维/环氧乙烯基酯树脂复合材料环境综合因素下的冲蚀行为及机制[J]. 复合材料学报, 2019, 36(9): 2059-2066.
[3] 罗英勤, 李华东, 洪明. 复合材料层合板振动特性基础研究综述[J]. 复合材料科学与工程, 2020(1): 114-119.
[4] 姚军, 姚起杭. 结构随机振动响应的工程简化分析[J]. 应用力学学报, 2002, 1(1):103-105.
[5] STEINWOLF A, RIZZI S A. Non-Gaussian analysis of turbulent boundary layer fluctuating pressure on aircraft skin panels[J]. Journal of Aircraft, 2006, 43(6): 1662-1675.
[6] VASSILOPOULOS A P, KELLER T. Fatigue of fiber-reinforced composites[M]. London: Springer, 2011.
[7] 韩京燮, 黄云峰, 张金民. 复合材料疲劳寿命预测[J]. 复合材料学报, 1987, 4(1): 16-24.
[8] 杨忠清, 姚卫星, 胡伟峰. 复合材料层合板疲劳寿命分析的系列单元失效模型[J]. 南京航空航天大学学报, 2007, 1(2): 6-10.
[9] 张文姣. 纤维增强复合材料的疲劳损伤模型及分析方法[D]. 哈尔滨: 哈尔滨工业大学, 2015.
[10] SANLITURK K Y, IMREGUN M. Fatigue life prediction using frequency response function[J]. Journal of Vibration and Acoustics, 1992, 114(7): 381-386.
[11] SARKANI S, MICHAELOV G, KIHL D P. Comparative study of nonlinear damage accumulation models in stochastic fatigue of frp laminates[J]. Journal of Structural Engineering, 2001, 127(3): 314-322.
[12] ZHOU S, SUN Y, GUO L. Random fatigue life prediction of carbon fibre-reinforced composite laminate based on hybrid time-frequency domain method[J]. Advanced Composite Materials,2017, 26(2): 181-195.
[13] BISHOP N W M. Vibration fatigue analysis in finite element environment[C]//The ⅩⅥ Encuentro Del Grupo Español de Fractura. Torremolinos. Spain: 1999: 14-16.
[14] HANNA Z A. Vibration fatigue assessment finite element analysis and test correlation[D]. Windsor: Unirversity of Windsor, 2005: 1-153.
[15] XIA J, YANG L, LIU Q, et al. Comparison of fatigue life prediction methods for solder joints under random vibration loading[J]. Microelectronics Reliability, 2019, 95: 58-64.
[16] STEINBERG D S. Vibration analysis for electronic equipment[M]. Wiley, 1988.
[17] WIRSCHING P H, LIGHT M C. Fatigue under wide band random stresses[J]. Journal of the Structural Division, 1980, 106(7): 1593-1607.
[18] 徐澧明, 范棋鑫, 蔡登安, 等. 平面整体冲破式易碎盖结构设计及有限元分析[J]. 上海航天(中英文), 2021, 38(1): 119-127.
[19] 矫桂琼, 贾普荣. 复合材料力学[M]. 西安: 西北工业大学出版社, 2008.
[20] HASHIN Z. Failure criteria for unidirectional fiber composites[J]. Journal of Applied Mechanics, 1980, 47(2): 329-334.
[21] CAMANHO P P, MATTHEWS F L. A progressive damage model for mechanically fastened joints in composite laminates[J]. Journal of Composite Materials, 1999, 33(24): 2248-2280.
[22] 姚卫星. 结构疲劳寿命分析[M]. 北京: 国防工业出版社, 2003.
[23] DIRLIK T. Application of computers in fatigue analysis[D]. Warwick University, 1985.
[24] GAO D, YAO Y, WEN W X, et al. Equivalent spectral method to estimate the fatigue life of composite laminates under random vibration loadings[J]. Mechanics of Composite Materials, 2021, 57(1): 101-114.