帮助 关于我们

返回检索结果

Coupled Bending–Bending–Axial–Torsional Vibrations of Rotating Blades

查看参考文献24篇

Liang Feng 1,2 *   Li Zhen 2   Yang Xiaodong 2 *   Zhang Wei 2   Yang Tianzhi 3  
文摘 In this paper,the coupled bending–bending–axial–torsional free vibrations of rotating blades are investigated based on the Euler–Bernoulli beam model.The coupled partial differential equations governing flapwise,edgewise,axial and torsional motions are derived by the Hamilton's principle,wherein three types of velocity-dependent terms,namely static centrifugal terms,dynamic centrifugal terms and gyroscopic coupling terms,are focused.The ordinary differential equations are acquired by the Galerkin truncation,and the natural frequencies in all directions and complex mode shapes of the rotating blades are analyzed in detail.It is revealed that the three types of velocity-dependent terms have different effects on the natural frequencies.The natural frequencies are noticeably dependent on the rotating speed and preset angle,except for the axial vibration,which is almost immune to the preset angle.The complex modal motions are displayed by a series of positions of the central line and free-end cross section for different time instants,showing the coupled vibrations among different directions.
来源 Acta Mechanica Solida Sinica ,2019,32(3):326-338 【核心库】
DOI 10.1007/s10338-019-00075-w
关键词 Rotating blades ; Coupled vibrations ; Gyroscopic coupling ; Complex modes ; Preset angle
地址

1. College of Mechanical Engineering,Yangzhou University, Yangzhou, 225127  

2. College of Mechanical Engineering and Applied Electronics,Beijing University of Technology, Beijing Key Laboratory of Nonlinear Vibrations and Strength of Mechanical Engineering, Beijing, 100124  

3. Department of Engineering Mechanics,Shenyang Aerospace University, Shenyang, 110136

语种 英文
文献类型 研究性论文
ISSN 0894-9166
学科 力学
基金 国家自然科学基金 ;  the Key Laboratory of Vibration and Control of Aero-Propulsion System Ministry of Education,Northeastern University ;  北京市自然科学基金
文献收藏号 CSCD:6522915

参考文献 共 24 共2页

1.  Hodges D H. A mixed variational formulation based on exact intrinsic equations for dynamics of moving beams. Int J Solids Struct,1990,26:1253-1273 被引 27    
2.  Cesnik C E S. Dynamic response of active twist rotor blades. Smart Mater Struct,2001,10:62-76 被引 2    
3.  Bendiksen O O. The effect of bending-torsion coupling on fan and compressor blade flutter. ASME J Eng Power,1982,104:617-623 被引 11    
4.  Cesnik C E S. VABS: A new concept for composite rotor blade cross-sectional modeling. J Am Helicopter Soc,1997,42:27-38 被引 12    
5.  Wright A D. Vibration modes of centrifugally stiffened beams. ASME J Appl Mech,1982,49:197-202 被引 14    
6.  Naguleswaran S. Lateral vibration of a centrifugally tensioned uniform Euler-Bernoulli beam. J Sound Vib,1994,176:613-624 被引 8    
7.  Du H. A power-series solution for vibration of a rotating Timoshenko beam. J Sound Vib,1994,175:505-523 被引 8    
8.  Sanchezhubert J. Coupling of bending-torsion-traction for anisotropic beams with heterogeneous section. Cr Acad Sci Ii,1991,312:337-344 被引 1    
9.  Banerjee J R. Free vibration of centrifugally stiffened uniform and tapered beams using the dynamic stiffness method. J Sound Vib,2000,233:857-875 被引 13    
10.  Chen W R. Transverse vibrations of a rotating twisted Timoshenko beam under axial loading. ASME J Vib Acoust,1993,115:285-294 被引 3    
11.  Genta G. A harmonic finite element for the analysis of flexural, torsional and axial rotordynamic behavior of blade arrays. J Sound Vib,1997,207:693-720 被引 4    
12.  Sivaneri N T. Dynamic stability of a rotor blade using finite-element analysis. AIAA J,1982,20:716-723 被引 8    
13.  Yang X D. Linear and nonlinear modal analysis of the axially moving continua based on the invariant manifold method. Acta Mech,2017,228:465-474 被引 3    
14.  Lin S C. Vibration analysis of a rotating Timoshenko beam. J Sound Vib,2001,240:303-322 被引 10    
15.  Lee S Y. Free vibrations of a rotating inclined beam. ASME J Appl Mech,2007,74:406-414 被引 2    
16.  Banerjee J R. Dynamic stiffness method for inplane free vibration of rotating beams including Coriolis effects. J Sound Vib,2014,333:7299-7312 被引 7    
17.  Chung J. Dynamic analysis of a rotating cantilever beam by using the finite element method. J Sound Vib,2002,249:147-164 被引 21    
18.  Kim H. Dynamic model for free vibration and response analysis of rotating beams. J Sound Vib,2013,332:5917-5928 被引 7    
19.  Pesheck E. Accurate reduced-order models for a simple rotor blade model using nonlinear normal modes. Math Comput Model,2001,33:1085-1097 被引 1    
20.  Huang C L. Free vibration analysis of rotating Euler beams at high angular velocity. Comput Struct,2010,88:991-1001 被引 7    
引证文献 2

1 Zhang Bo Subharmonic and Combination Resonance of Rotating Pre-deformed Blades Subjected to High Gas Pressure Acta Mechanica Solida Sinica,2020,33(5):635-649
被引 2

2 Liu Yunfei Multiple internal resonances of rotating composite cylindrical shells under varying temperature fields Applied Mathematics and Mechanics,2022,43(10):1543-1554
被引 0 次

显示所有2篇文献

论文科学数据集
PlumX Metrics
相关文献

 作者相关
 关键词相关
 参考文献相关

版权所有 ©2008 中国科学院文献情报中心 制作维护:中国科学院文献情报中心
地址:北京中关村北四环西路33号 邮政编码:100190 联系电话:(010)82627496 E-mail:cscd@mail.las.ac.cn 京ICP备05002861号-4 | 京公网安备11010802043238号