上海交通大学学报 ›› 2024, Vol. 58 ›› Issue (4): 428-437.doi: 10.16183/j.cnki.jsjtu.2022.396
收稿日期:
2022-10-08
修回日期:
2022-12-18
接受日期:
2023-01-06
出版日期:
2024-04-28
发布日期:
2024-04-30
通讯作者:
何泽青,高级工程师;E-mail:zqhe@aoe.ac.cn.
作者简介:
黄 涛(1997-),硕士生,从事飞行器结构动力学研究.
HUANG Tao1,2, HE Zeqing1,2(), SONG Lin1
Received:
2022-10-08
Revised:
2022-12-18
Accepted:
2023-01-06
Online:
2024-04-28
Published:
2024-04-30
摘要:
根据达朗贝尔原理建立圆柱状薄膜非线性振动方程并对其展开分析与试验验证.建立圆柱膜振动问题的控制方程组,依据薄膜振动物理方程与边界条件简化方程组并求解;得到圆柱膜非线性振动频率解析解,并通过有限元仿真对其线性解析解进行验证.结果表明,理论计算与数值仿真结果误差较小,有限元方法适用于柔性薄膜结构模态分析.采用三维激光扫描式测振系统测试圆柱膜在空气环境中的振动频率,利用有限元分析软件获得圆柱膜干模态和湿模态振动频率并提取空气附加质量系数.结果表明,圆柱膜振动湿模态测试结果与数值分析结果具有良好的一致性,地面空气附加质量对圆柱膜振动的影响与薄膜自身质量处于同一量级.
中图分类号:
黄涛, 何泽青, 宋林. 圆柱薄膜振动特性[J]. 上海交通大学学报, 2024, 58(4): 428-437.
HUANG Tao, HE Zeqing, SONG Lin. Vibration Characteristics of Cylindrical Membrane[J]. Journal of Shanghai Jiao Tong University, 2024, 58(4): 428-437.
[1] |
黄宛宁, 张晓军, 李智斌, 等. 临近空间科学技术的发展现状及应用前景[J]. 科技导报, 2019, 37(21): 46-62.
doi: 10.3981/j.issn.1000-7857.2019.21.005 |
HUANG Wanning, ZHANG Xiaojun, LI Zhibin, et al. Development status and application prospect of near space science and technology[J]. Science & Technology Review, 2019, 37(21): 46-62. | |
[2] | 邱慧, 李潇, 樊俊峰, 等. 航天器平面薄膜结构模态分析和试验[J]. 航天器工程, 2017, 26(3): 43-49. |
QIU Hui, LI Xiao, FAN Junfeng, et al. Modal analysis and experiment of spacecraft flat membrane structures[J]. Spacecraft Engineering, 2017, 26(3): 43-49. | |
[3] | 张祎贝, 陈务军, 谢超, 等. 大尺度空间薄膜地面振动试验网格膜等效理论分析与数值模拟[J]. 载人航天, 2019, 25(4): 419-424. |
ZHANG Yibei, CHEN Wujun, XIE Chao, et al. Equivalent theoretical analysis and numerical simulation of grid membrane for large-scale space film ground vibration test[J]. Manned Spaceflight, 2019, 25(4): 419-424. | |
[4] | XIAO W W, CHEN W J, FU G Y. Wrinkle analysis of the space inflatable paraboloid antenna[J]. Journal of Shanghai Jiao Tong University (Science), 2011, 16(1): 24-33. |
[5] |
张宇, 王晓亮. 基于显式动力学的软式飞艇流固耦合计算框架[J]. 上海交通大学学报, 2021, 55(3): 311-319.
doi: 10.16183/j.cnki.jsjtu.2019.351 |
ZHANG Yu, WANG Xiaoliang. Fluid-structure interaction calculation framework for non-rigid airship based on explicit dynamics[J]. Journal of Shanghai Jiao Tong University, 2021, 55(3): 311-319. | |
[6] | TATEMATSU Y, SUZUKI T, YAMAZAKI M, et al. Verification of the similarity rules for spin deployment membrane in the ground experiment[C]// The 4th AIAA Spacecraft Structures Conference. Washington D. C., USA: American Institute of Aeronautics and Astronautics, 2017: 1114-1126. |
[7] | 陈宇峰, 陈务军, 何艳丽, 等. 柔性飞艇主气囊干湿模态分析与影响因素[J]. 上海交通大学学报, 2014, 48(2): 234-238. |
CHEN Yufeng, CHEN Wujun, HE Yanli, et al. Dry and wet modal analysis and evaluation of influencing factors for flexible airship envelop[J]. Journal of Shanghai Jiao Tong University, 2014, 48(2): 234-238. | |
[8] | 张祎贝, 陈务军, 邓小伟, 等. 薄膜结构空气与低真空环境下模态辨识仿真及试验[J]. 振动与冲击, 2020, 39(20): 168-174. |
ZHANG Yibei, CHEN Wujun, DENG Xiaowei, et al. Simulation and experiment for membrane modal identification in the air and low vacuum environment[J]. Journal of Vibration and Shock, 2020, 39(20): 168-174. | |
[9] | LI Y Q, WANG L, SHEN Z Y, et al. Added-mass estimation of flat membranes vibrating in still air[J]. Journal of Wind Engineering & Industrial Aerodynamics, 2011, 99(8): 815-824. |
[10] | 何泽青, 张冬辉, 宋林, 等. 正交异性薄膜非线性振动分析[J]. 振动与冲击, 2018, 37(12): 252-259. |
HE Zeqing, ZHANG Donghui, SONG Lin, et al. Nonlinear vibration analysis of orthotropic membrane[J]. Journal of Vibration and Shock, 2018, 37(12): 252-259. | |
[11] | TIMOSHENKO S, YOUNG S H, WEAVER W. Vibration problems in engineering[M]. 4th ed. New York,USA: John Wiley & Sons, 1974. |
[12] |
LEE N, LEE S, CHO H, et al. Effect of flexibility on flapping wing characteristics in hover and forward flight[J]. Computers & Fluids, 2018, 173: 111-117.
doi: 10.1016/j.compfluid.2018.03.017 URL |
[13] | 杨兆臣, 张怀新. 基于双向流固耦合的柔性表面覆盖层减阻性能[J]. 上海交通大学学报, 2016, 50(8): 1165-1172. |
YANG Zhaochen, ZHANG Huaixin. Investigation of drag reduction of flexible surface based on bi-directional fluid-struction interaction[J]. Journal of Shanghai Jiao Tong University, 2016, 50(8): 1165-1172. | |
[14] | 毛丽娜, 谭惠丰. 充气天线反射面结构的理论分析与精度预测[J]. 工程力学, 2010, 27(4): 197-201. |
MAO Lina, TAN Huifeng. Stucuture analysis and precision evaluation of inflatable antenna reflector[J]. Engineering Mechanics, 2010, 27(4): 197-201. | |
[15] | SOARCE M. Application of finite difference equations to shell analysis[M]. Oxford, UK: Pergamon Press, 1967. |
[16] | 邵琦, 陆一凡, 史创, 等. 空间薄膜结构刚柔耦合非线性动力学分析[J]. 中国空间科学技术, 2022, 42(1): 47-56. |
SHAO Qi, LU Yifan, SHI Chuang, et al. Rigid-flexible coupled nonlinear dynamics and analysis of space membrane structure[J]. Chinese Space Science and Technology, 2022, 42(1): 47-56. | |
[17] |
刘人怀, 薛江红. 复合材料层合板壳非线性力学的研究进展[J]. 力学学报, 2017, 49(3): 487-506.
doi: 10.6052/0459-1879-16-253 |
LIU Renhuai, XUE Jianghong. Development of nonlinear mechanics for laminated composite plates and shells[J]. Chinese Journal of Theoretical and Applied Mechanics, 2017, 49(3): 487-506.
doi: 10.6052/0459-1879-16-253 |
|
[18] | WU H X, WU R X, MA T F, et al. A nonlinear analysis of surface acoustic waves in isotropic elastic solids[J]. Theoretical & Applied Mechanics Letters, 2022, 12(2): 98-103. |
[19] |
MAHERI M R, SEVERN R T. Experimental added-mass in modal vibration of cylindrical structures[J]. Engineering Structures, 1992, 14(3): 163-175.
doi: 10.1016/0141-0296(92)90027-N URL |
[1] | 张波涛,朱晔晨,梅勇,龚圣捷. 平直条带流致振动特性实验及其数值模拟研究[J]. 上海交通大学学报, 2020, 54(1): 100-105. |
[2] | 任晨辉,杨德庆. 余弦形预制双曲梁非线性隔振器的隔振性能[J]. 上海交通大学学报, 2019, 53(7): 852-859. |
[3] | 陈宇峰,陈务军,何艳丽,张大旭. 柔性飞艇主气囊干湿模态分析与影响因素[J]. 上海交通大学学报(自然版), 2014, 48(02): 234-238. |
阅读次数 | ||||||
全文 |
|
|||||
摘要 |
|
|||||