Natural characteristics calculation and analysis of fiber reinforced truncated conical shell
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摘要:
以理论与实践相结合的方式分析了纤维增强截顶圆锥壳的固有特性。针对纤维增强复合圆锥壳的结构特性引入半锥角系数,考虑复合结构各向异性的影响,基于经典层合理论对其进行了理论建模;利用Rayleigh-Ritz法和正交多项式法求解了结构的固有特性。通过搭建相应的实验系统,以TC300/环氧树脂复合圆锥壳为研究对象进行测试,结果表明:该方法所获得固有频率的结果与试验测试结果间的误差在1.4%~2.3%之间,进而验证了所提出模型的正确性。最后,讨论了半锥角大小、不同约束方式和不同纤维铺层角度等参数对结构固有特性的影响规律。
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关键词:
- 纤维增强复合结构 /
- 截顶圆锥壳 /
- 固有特性 /
- Rayleigh-Ritz法 /
- 正交多项式
Abstract:The natural characteristics of composite conical shells were calculated and verified by combining theory and experiment. Based on the classical lamination theory and considering the influence of anisotropy of composite structures, the theoretical model was established by introducing half-cone angle coefficients. Then, the natural characteristics of the structures were obtained by utilizing the Rayleigh-Ritz method and orthogonal polynomial method. A natural characteristic experiment system of TC300/epoxy resin composite conical shell was established and the natural characteristics were acquired. The results showed that the error between the calculated and test results was between 1.4% and 2.3%, which further verified the correctness of the proposed model. Finally, the influences of different parameters, such as the half cone angle, the boundary conditions and the fiber ply angles, on the natural characteristics of the structure were discussed.
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表 1 计算和测试获得的纤维增强截顶圆锥壳的前3阶固有频率和模态振型
Table 1. Calculation and testing of the first seventh-order intrinsic frequencies and modal shapes of thin fiber-metal composite shells obtained
参数 模态阶次 1 2 3 频率/Hz 实验频率A 716.22 1 217.30 1 670.10 Matlab计算频率B 705.23 1 246.16 1 645.50 Ansys计算频率C 726.28 1 157.70 1 756.90 误差/% |A−B|/B 1.5 2.3 1.4 |A−C|/C 1.3 5.1 4.9 |B−C|/B 2.9 7.1 6.7 振型图 Matlab 


Ansys 


表 2 不同半锥角下的纤维增强截顶圆锥壳固有频率
Table 2. Natural frequencies of fiber reinforced truncated conical shell with different semi-conical angle
α/(°) 频率相关参数 模态阶次 1 2 3 4 5 6 0 频率/Hz A1(Matlab) 977.92 1 637.82 1 953.57 2 284.71 2 796.62 3 166.14 B1(Ansys) 923.48 1 583.40 1 884.50 2 312.70 2 845.30 3 094.80 误差/% |A1−B1|/A1 5.5 3.3 3.5 1.2 1.7 2.3 30 频率/Hz A2(Matlab) 705.23 1 246.16 1 645.50 1 934.49 2 450.27 2 864.31 B2(Ansys) 726.28 1 157.70 1 756.90 1 987.60 2 412.20 2 764.30 误差/% |A2−B2|/A2 2.9 7.1 6.7 2.7 1.6 3.5 60 频率/Hz A3(Matlab) 436.22 954.84 1 361.34 1 799.95 2 116.60 2 54869 B3(Ansys) 414.51 1 002.70 1 271.30 1 844.80 2 199.10 2 516.10 误差/% |A3−B3|/A3 5.0 5.0 6.6 2.5 3.9 1.3 90 频率/Hz A4(Matlab) 143.65 642.99 1 049.54 1 381.93 1 867.34 2 212.62 B4(Ansys) 138.94 611.34 992.77 1 422.30 1 912.60 2 185.70 误差/% |A4−B4|/A4 3.3 4.9 5.4 3.1 2.4 1.2 表 3 不同固定端下纤维增强截顶圆锥壳的固有频率
Table 3. Natural frequencies of fiber reinforced truncated conical shell under different boundary conditions
固定方式 频率相关参数 模态阶次 1 2 3 4 5 6 小端固定 频率/Hz A1(Matlab) 366.42 595.88 994.26 1 290.31 1 455.60 1 831.46 B1(Ansys) 348.33 618.74 1 022.20 1 272.10 1 489.60 1 795.50 误差/% |A1−B1|/A1 4.9 3.8 2.8 1.4 2.3 1.9 大端固定 频率/Hz A2(Matlab) 705.23 1 246.16 1 645.50 1 934.49 2 450.27 2 864.31 B2(Ansys) 726.28 1 157.70 1 756.90 1 987.60 2 412.20 2 764.30 误差/% |A2−B2|/A2 2.9 7.1 6.7 2.7 1.6 3.5 两端固定 频率/Hz A3(Matlab) 1 012.72 1 368.45 1 746.77 2 106.82 2 341.16 2 623.42 B3(Ansys) 998.54 1 390.50 1 774.50 2 081.90 2 323.70 2 658.50 误差/% |A3−B3|/A3 1.4 1.6 1.6 1.2 0.7 1.3 两端自由 频率/Hz A4(Matlab) 124.16 216.34 314.59 475.38 598.73 715.64 B4(Ansys) 116.27 208.01 298.75 441.21 618.40 740.44 误差/% |A4−B4|/A4 6.3 3.8 5.0 7.1 3.2 3.4 表 4 不同铺层角度下纤维增强截顶圆锥壳的固有频率
Table 4. Natural frequencies of fiber reinforced truncated conical shell with different laid methods
铺层角度 频率相关参数 模态阶次 1 2 3 4 5 6 [0°/90°]s 频率/Hz A1(Matlab) 441.94 987.35 1 435.64 1 895.46 2 334.71 2 791.86 B1(Ansys) 422.57 1 002.42 1 519.20 1 822.80 2 284.70 2 680.20 误差/% |A1−B1|/A1 4.3 1.5 5.5 3.8 2.1 3.9 [+45°/−45°]s 频率/Hz A2(Matlab) 705.23 1 246.16 1 645.50 1 934.49 2 450.27 2 864.31 B2(Ansys) 726.28 1 157.70 1 756.90 1 987.60 2 412.20 2 764.30 误差/% |A2−B2|/A2 2.9 7.1 6.7 2.7 1.6 3.5 [90°/90°]s 频率/Hz A3(Matlab) 912.34 1 132.60 1 455.74 1 725.34 2 236.68 2 886.43 B3(Ansys) 955.34 1 160.50 1 500.10 1 795.30 2 331.00 1 986.40 误差/% |A3−B3|/A3 4.7 2.4 3.0 4.0 4.2 3.1 -
[1] 曹志远. 板壳振动理论[M]. 北京: 中国铁道出版社,1989. CAO Zhiyuan. Vibration theory of plate and shell[M]. Beijing: China Railway Publishing House,1989. (in ChineseCAO Zhiyuan. Vibration theory of plate and shell[M]. Beijing: China Railway Publishing House, 1989. (in Chinese) [2] QATU M S. Vibration of laminated shells and plates[M]. Amsterdam,Holland: Elsevier,2004: 259-320. [3] 邢誉峰,刘波. 板壳自由振动的精确解[M]. 北京: 科学出版社,2015. XING Yufeng,LIU Bo. Exact solutions of free vibrations of plates and shells[M]. Beijing: Science Press,2015. (in ChineseXING Yufeng, LIU Bo. Exact solutions of free vibrations of plates and shells[M]. Beijing: Science Press, 2015. (in Chinese) [4] ZOU Y,TONG L,STEVEN G P. Vibration-based model-dependent damage (delamination) identification and health monitoring for composite structures: a review[J]. Journal of Sound and Vibration,2000,230(2): 357-378. doi: 10.1006/jsvi.1999.2624 [5] 李晖,孙伟,许卓,等. 纤维增强复合薄板振动测试与分析方法[M]. 北京: 机械工业出版社,2020. LI Hui,SUN Wei,XU Zhuo,et al. Vibration test and analysis method of fiber reinforced composite thin plate[M]. Beijing: China Machine Press,2020. (in ChineseLI Hui, SUN Wei, XU Zhuo, et al. Vibration test and analysis method of fiber reinforced composite thin plate[M]. Beijing: China Machine Press, 2020. (in Chinese) [6] 张德众. 叠层复合材料旋转薄壳的自由振动[J]. 振动与冲击,1985,4(1): 28-37. ZHANG Dezhong. Free vibration of thin-wall shells of revolution of laminated composites[J]. Journal of Vibration and Shock,1985,4(1): 28-37. (in ChineseZHANG Dezhong. Free vibration of thin-wall shells of revolution of laminated composites[J]. Journal of Vibration and Shock, 1985, 4(1): 28-37. (in Chinese) [7] 张德众,孟凡平. 叠层复合材料旋转薄壳的半有限元分析[J]. 山东工业大学学报,1986,16(6): 41-47. ZHANG Dezhong,MENG Fanping. Half-finite element analysis of laminated composite thin-wall shells of revolution[J]. Journal of Shandong University (Engineering Science),1986,16(6): 41-47. (in ChineseZHANG Dezhong, MENG Fanping. Half-finite element analysis of laminated composite thin-wall shells of revolution[J]. Journal of Shandong University (Engineering Science), 1986, 16(6): 41-47. (in Chinese) [8] TONG Liyong. Free vibration of composite laminated conical shells[J]. International Journal of Mechanical Sciences,1993,35(1): 47-61. doi: 10.1016/0020-7403(93)90064-2 [9] 朱显明,张国良,师汉民. 截顶圆锥壳体的自由振动分析[J]. 舰船科学技术,1997,19(5): 33-36. ZHU Xianming,ZHANG Guoliang,SHI Hanmin. Free vibration analysis of truncated conical shell[J]. Ship Science and Technology,1997,19(5): 33-36. (in ChineseZHU Xianming, ZHANG Guoliang, SHI Hanmin. Free vibration analysis of truncated conical shell[J]. Ship Science and Technology, 1997, 19(5): 33-36. (in Chinese) [10] LIANG Sen,CHEN H L,CHEN Tianning,et al. The natural vibration of a symmetric cross-ply laminated composite conical-plate shell[J]. Composite Structures,2007,80(2): 265-278. doi: 10.1016/j.compstruct.2006.05.014 [11] TRIPATHI V,SINGH B N,SHUKLA K K. Free vibration of laminated composite conical shells with random material properties[J]. Composite Structures,2007,81(1): 96-104. doi: 10.1016/j.compstruct.2006.08.002 [12] QU Yegao,LONG Xinhua,WU Shihao,et al. A unified formulation for vibration analysis of composite laminated shells of revolution including shear deformation and rotary inertia[J]. Composite Structures,2013,98: 169-191. doi: 10.1016/j.compstruct.2012.11.001 [13] VIOLA E,TORNABENE F,FANTUZZI N. General higher-order shear deformation theories for the free vibration analysis of completely doubly-curved laminated shells and panels[J]. Composite Structures,2013,95: 639-666. doi: 10.1016/j.compstruct.2012.08.005 [14] 瞿叶高,华宏星,谌勇,等. 复合材料旋转壳自由振动分析的新方法[J]. 力学学报,2013,45(1): 139-143. QU Yegao,HUA Hongxing,CHEN Yong,et al. A new method for free vibration analysis of composite laminated shelles of revolution[J]. Chinese Journal of Theoretical and Applied Mechanics,2013,45(1): 139-143. (in ChineseQU Yegao, HUA Hongxing, CHEN Yong, et al. A new method for free vibration analysis of composite laminated shelles of revolution[J]. Chinese Journal of Theoretical and Applied Mechanics, 2013, 45(1): 139-143. (in Chinese) [15] XIE Xiang,JIN Guoyong,LI Wanyou,et al. A numerical solution for vibration analysis of composite laminated conical,cylindrical shell and annular plate structures[J]. Composite Structures,2014,111: 20-30. doi: 10.1016/j.compstruct.2013.12.019 [16] SU Zhu,JIN Guoyong,SHI Shuangxia,et al. A unified solution for vibration analysis of functionally graded cylindrical,conical shells and annular plates with general boundary conditions[J]. International Journal of Mechanical Sciences,2014,80: 62-80. doi: 10.1016/j.ijmecsci.2014.01.002 [17] DEY S,MUKHOPADHYAY T,KHODAPARAST H H,et al. Stochastic natural frequency of composite conical shells[J]. Acta Mechanica,2015,226(8): 2537-2553. doi: 10.1007/s00707-015-1316-4 [18] 宋旭圆. 层合薄壁圆柱壳结构的非线性振动特性研究[D]. 辽宁 大连: 大连理工大学,2016. SONG Xuyuan. Nonlinear vibration characteristics of laminated thin-walled cylindrical shell[D]. Dalian Liaoning: Dalian University of Technology,2016. (in ChineseSONG Xuyuan. Nonlinear vibration characteristics of laminated thin-walled cylindrical shell[D]. Dalian Liaoning: Dalian University of Technology, 2016. (in Chinese) [19] 周正学,李晖,薛鹏程,等. 纤维增强复合薄壳固有特性计算及验证[J]. 中国机械工程,2018,29(10): 1234-1239. ZHOU Zhengxue,LI Hui,XUE Pengcheng,et al. Natural characteristic calculation and verification of FRCS[J]. China Mechanical Engineering,2018,29(10): 1234-1239. (in ChineseZHOU Zhengxue, LI Hui, XUE Pengcheng, et al. Natural characteristic calculation and verification of FRCS[J]. China Mechanical Engineering, 2018, 29(10): 1234-1239. (in Chinese) [20] ZHANG Hong,ZHU Rupeng,SHI Dongyan,et al. A simplified plate theory for vibration analysis of composite laminated sector,annular and circular plate[J]. Thin-Walled Structures,2019,143: 106252. doi: 10.1016/j.tws.2019.106252 [21] SAFARPOUR M,RAHIMI A R,ALIBEIGLOO A. Static and free vibration analysis of graphene platelets reinforced composite truncated conical shell,cylindrical shell,and annular plate using theory of elasticity and DQM[J]. Mechanics Based Design of Structures and Machines,2020,48(4): 496-524. doi: 10.1080/15397734.2019.1646137 [22] SOBHANI E,MASOODI A R,AHMADI-PARI A R. Vibration of FG-CNT and FG-GNP sandwich composite coupled Conical-Cylindrical-Conical shell[J]. Composite Structures,2021,273: 114281. doi: 10.1016/j.compstruct.2021.114281 [23] NIU Yan,YAO Minghui. Linear and nonlinear vibrations of graphene platelet reinforced composite tapered plates and cylindrical panels[J]. Aerospace Science and Technology,2021,115: 106798. doi: 10.1016/j.ast.2021.106798 [24] 田宏业,刘朋,胡志宽,等. 基于半解析法的功能梯度圆锥板自由振动特性[J]. 船舶力学,2021,25(3): 351-359. TIAN Hongye,LIU Peng,HU Zhikuan,et al. Free vibration characteristics of functionally graded conical panels with complex boundary conditions[J]. Journal of Ship Mechanics,2021,25(3): 351-359. (in ChineseTIAN Hongye, LIU Peng, HU Zhikuan, et al. Free vibration characteristics of functionally graded conical panels with complex boundary conditions[J]. Journal of Ship Mechanics, 2021, 25(3): 351-359. (in Chinese) [25] 夏鑫. 硬涂层阻尼薄壁截锥壳的固有特性及相似动力学研究[D]. 辽宁 鞍山: 辽宁科技大学,2021. XIA Xin. Natural characteristics and similar dynamics of thin-walled truncated conical shell with hard coating damping[D]. Anshan Liaoning: University of Science and Technology Liaoning,2021. (in ChineseXIA Xin. Natural characteristics and similar dynamics of thin-walled truncated conical shell with hard coating damping[D]. Anshan Liaoning: University of Science and Technology Liaoning, 2021. (in Chinese) [26] MAHI A,BEDIA E A A,TOUNSI A. A new hyperbolic shear deformation theory for bending and free vibration analysis of isotropic,functionally graded,sandwich and laminated composite plates[J]. Applied Mathematical Modelling,2015,39(9): 2489-2508. doi: 10.1016/j.apm.2014.10.045 -

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