Nonlinear vibration analysis of rotating beams undergoing parametric instability: Lagging-axial motion

被引:45
作者
Arvin, Hadi [1 ]
Arena, Andrea [2 ]
Lacarbonara, Walter [2 ]
机构
[1] Shahrekord Univ, Fac Engn, Shahrekord 115, Iran
[2] Sapienza Univ Rome, Dept Struct & Geotech Engn, I-00184 Rome, Italy
关键词
Rotating beams; Nonlinear free vibrations; Coriolis force; Method of multiple scales; Effective nonlinearity coefficient; Parametric resonance; HELICOPTER ROTOR BLADES; STABILITY; FORMULATION; EQUATIONS; FLEXURE; TORSION; SPEED;
D O I
10.1016/j.ymssp.2020.106892
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
The nonlinear free vibration and principal parametric resonance of rotating beams are investigated taking into account the lagging-axial coupling motion due to Coriolis force. This work tackles analytically the problem of parametric resonances induced by periodic modulation of the angular speed. The nonlinear equations of motion are obtained via a direct Lagrangian formulation. The method of multiple scales is employed to perform a perturbation analysis of the nondimensional equations of motion to deliver the effective nonlinearity of the lagging and axial modes and the critical conditions for the onset of parametric resonances. A comprehensive study on the effect of the rotational speed and the damping ratio on the modes nonlinearity and on the instability regions is presented. Comparisons in terms of effective nonlinearity coefficient and principal parametric resonance response were carried out so as to illustrate the importance of the exact geometrical formulation against ad hoc beam theories such as the Euler-Bernoulli beam model. (C) 2020 Elsevier Ltd. All rights reserved.
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页数:21
相关论文
共 27 条
[1]   Enhancing flutter stability in nanocomposite thin panels by harnessing CNT/polymer dissipation [J].
Arena, Andrea ;
Talo, Michela ;
Snyder, Matthew P. ;
Lacarbonara, Walter .
MECHANICS RESEARCH COMMUNICATIONS, 2020, 104
[2]   Nonlinear Aeroelastic Formulation and Postflutter Analysis of Flexible High-Aspect-Ratio Wings [J].
Arena, Andrea ;
Lacarbonara, Walter ;
Marzocca, Pier .
JOURNAL OF AIRCRAFT, 2013, 50 (06) :1748-1764
[3]   Nonlinear free vibration analysis of rotating composite Timoshenko beams [J].
Arvin, H. ;
Bakhtiari-Nejad, F. .
COMPOSITE STRUCTURES, 2013, 96 :29-43
[4]   On Parametrically Excited Vibration and Stability of Beams with Varying Rotating Speed [J].
Arvin, Hadi .
IRANIAN JOURNAL OF SCIENCE AND TECHNOLOGY-TRANSACTIONS OF MECHANICAL ENGINEERING, 2019, 43 (02) :177-185
[5]   Dynamic stability in principal parametric resonance of rotating beams: Method of multiple scales versus differential quadrature method [J].
Arvin, Hadi ;
Tang, You-Qi ;
Nadooshan, Afshin Ahmadi .
INTERNATIONAL JOURNAL OF NON-LINEAR MECHANICS, 2016, 85 :118-125
[6]   A fully nonlinear dynamic formulation for rotating composite beams: Nonlinear normal modes in flapping [J].
Arvin, Hadi ;
Lacarbonara, Walter .
COMPOSITE STRUCTURES, 2014, 109 :93-105
[7]   A geometrically exact approach to the overall dynamics of elastic rotating blades-part 2: flapping nonlinear normal modes [J].
Arvin, Hadi ;
Lacarbonara, Walter ;
Bakhtiari-Nejad, Firooz .
NONLINEAR DYNAMICS, 2012, 70 (03) :2279-2301
[8]   Nonlinear equations of flexural-flexural-torsional oscillations of rotating beamswith arbitrary cross-section [J].
Avramov, K. V. ;
Pierre, C. ;
Shyriaieva, N. V. .
INTERNATIONAL APPLIED MECHANICS, 2008, 44 (05) :582-589
[9]  
DASILVA MRMC, 1986, VERTICA, V10, P171
[10]  
DASILVA MRMC, 1986, VERTICA, V10, P151