Prediction of micro-macro damping characteristics of laminated composite cylindrical shells
DAI Qiyi1,2, QIN Zhaoye2, CHU Fulei2
1. Department of Mechanical Engineering, Beijing Technology and Business University, Beijing 100048, China;
2. Department of Mechanical Engineering, Tsinghua University, Beijing 100084, China
Abstract:Micro-macro damping characteristics of laminated composite cylindrical shells were studied here. Based on Reissner-Naghdi thin shell theory, the vibration differential equations of a cylindrical shell were derived. In process of separation of variables, Haar wavelet series was used to represent axial mode, and Fourier series was used to represent circumferential mode. The unknown coefficients appearing in integration were solved using boundary conditions to obtain the characteristic equation to be used for analyzing free vibration characteristics of the cylindrical shell. Based on the microscopic damping calculation method and multi-cell model of hybrid materials, the equivalent damping characteristics and equivalent elastic characteristics of single-layer composite material were obtained, and damping characteristics of a composite cylindrical shell were predicted using the complex modulus method. By comparing damping prediction results with those published in other literature, the effectiveness of the proposed method was verified. Effects of fiber content, circumferential wave number, laminated mode and geometric parameters on damping characteristics of composite cylindrical shell under four typical boundary conditions were further analyzed.
[1]温登哲. 航空发动机机匣模型的若干动力学特性研究[D]. 哈尔滨: 哈尔滨工业大学, 2015.
[2]李志敏. 船舶与海洋工程中复合材料圆柱壳结构屈曲和后屈曲行为研究[D]. 上海: 上海交通大学, 2008.
[3]陈烈民, 杨宝宁. 复合材料的力学分析[M]. 北京: 中国科学技术出版社, 2006.
[4]ALAM N, ASNANI N T. Vibration and damping analysis of a multilayered cylindrical shell, I: theoretical analysis[J]. AIAA Journal, 1984, 22(6): 803-810.
[5]SINGH S P, GUPTA K. Free damped flexural vibration analysis of composite cylindrical tubes using beam and shell theories[J]. Journal of Sound and Vibration, 1994, 172(2): 171-190.
[6]SINGH S P, GUPTA K. Damped free vibrations of layered composite cylindrical shells[J]. Journal of Sound and Vibration, 1994, 172(2): 191-209.
[7]HUFENBACH W, HOLSTE C, KROLL L. Vibration and damping behaviour of multi-layered composite cylindrical shells[J]. Composite Structures, 2002, 58: 165-174.
[8]CHATE A, RIKARDS R, KORJAKIN A. Analysis of free damped vibrations of laminated composite cylindrical shells[J]. Mechanics of Composite Materials, 1995, 31(5):474-484.
[9]SARAVANOS D A, VARELIS D, PLAGIANAKOS T S, et al. A shear beam finite element for the damping analysis of tubular laminated composite beams[J]. Journal of Sound and Vibration, 2006, 291(3/4/5): 802-823.
[10]白宇杰, 张小章. 基于波动法的复合材料圆柱壳阻尼特性分析[J]. 振动与冲击, 2014, 33(9): 111-115.
BAI Yujie, ZHANG Xiaozhang. Damping behavior analysis of composite cylindrical shells using wave approach[J]. Journal of Vibration and Shock, 2014, 39(9):111-115.
[11]白宇杰. 复合材料圆柱壳动力学分析及损伤研究[D]. 北京:清华大学,2016.
[12]DAI Q Y, CAO Q J, CHEN Y S. Frequency analysis of rotating truncated conical shells using the Haar wavelet method[J]. Applied Mathematical Modelling, 2018, 57: 603-613.
[13]XIE X, JIN G Y, YAN Y Q, et al. Free vibration analysis of composite laminated cylindrical shells using the Haar wavelet method[J]. Composite Structures, 2014, 109: 169-177.
[13]MURTHY P L N. Second generation integrated compositeanalyzer(ICAN) computer code[R].Washington,DC:NASA,1993.
[14]DAI Q Y, CAO Q J. Parametric instability analysis of truncated conical shells using the Haar wavelet method[J]. Mechanical Systems and Signal Processing,2018, 105: 200-213.
[15]SARAVANOS D A, CHAMIS C C. Unified micromechanics of damping for unidirection and off-axis fiber composites[J]. Journal Composites Technology & Research, 1990, 12(1): 31-40.
[16]KALISKE M, ROTHERT H. Damping characterization of unidirectional fibre reinforced polymer composites[J]. Composites Engineering, 1995, 5(5):551-567.