Comparison of two iteration procedures for a class of nonlinear jerk equations

A modified Michens iteration procedure and a direct Michens iteration procedure are applied to determine approximate periods and analytical approximate periodic solutions of a class of nonlinear jerk equations. When we use the modified Michens iteration procedure to deal with the nonlinear jerk equations, we need to solve the nonlinear algebra equation for determining the approximate angular frequency. The higher the number of iterations, the more difficult it is to deal with the nonlinear algebra equation. This is because the kth-order approximate solution obtained by the modified Michens iteration procedure is a function of the angular frequency. However, since the kth-order approximate solution obtained by the direct Michens iteration procedure is independent on the kth-order approximate angular frequency, the form of nonlinear algebra equation that determines the kth-order approximate angular frequency of nonlinear jerk equation is similar. The second-order approximate period obtained by the direct Michens iteration procedure provides very accurate results for the large initial velocity amplitudes. But the second-order approximate period obtained by the modified Michens iteration procedure is invalid for all amplitudes B of the initial velocity. A comparison of the first- and second-order approximate periodic solutions obtained by the direct Michens iteration procedure with the numerically exact solutions shows that the second-order approximate periodic solution is much more accurate than the first one. Thus, the direct Michens iteration procedure is very effective for the class of nonlinear jerk equations.     

Does vibration amplitude influence the evaluation of nonlocal small scale parameter of single layered graphene sheets?

ABSTRACT

This study aims to evaluate the nonlocal small scale parameter for large amplitude vibration of single layered graphene sheets (SLGSs) comparing nonlinear resonant frequencies obtained via nonlocal continuum and molecular dynamics (MD) simulations. Nonlinear governing equations of motion are numerically solved employing the pseudo-spectral method to obtain the frequency response. Results reveal that the calibrated small scale parameter decreases when the vibration amplitude increases. Also, from MD simulations it is seen that for all length sizes after an ultimate vibration amplitude around 31% length size, the graphene sheets start to fracture.     

轴向运动超薄梁的非局部动力学分析

基于非局部弹性理论,建立了两端受初始张力的轴向运动超薄梁横向振动的控制方程。与现有的一些仅仅在控制方程中考虑非局部效应的研究不同,该文同时将非局部效应引入到两种典型的边界条件中,考察了非局部参数对超薄梁横向振动行为尤其是固有频率和临界速度的影响。结果表明:超薄性使得轴向运动梁的自由振动固有频率及临界速度降低,经典弹性理论高估了纳米尺度结构的弯曲刚度,轴向运动超薄梁的动力学行为存在明显的非局部尺寸效应。     

简支圆板非线性热弹耦合振动问题的研究

对温度场中周边简支圆板的轴对称非线性热弹耦合自由振动问题,运用伽辽金法求解, 得出一个关于时间的非线性常微分方程组,求出振幅随时间变化的数值解。将热弹耦合与非 热弹耦合情况进行对比,发现振幅较小时,热弹耦合效应使板的固有频率相对于无热弹耦合 情形提高：振幅较大时,热弹耦合效应使固有频率降低。本文还比较了不同热弹耦合参数对 应的振动情况。     

Exact solution for free vibration of coupled double viscoelastic graphene sheets by viscoPasternak medium

Based on nonlocal theory, this article discusses vibration of CDVGS¹ systems. The properties of each single layer graphene sheet (SLGS) are assumed to be orthotropic and viscoelastic. The two SLGSs are simply supported and coupled by an enclosing viscoelastic medium which is simulated as a Visco-Pasternak layer. This model is aimed at representing dynamic interactions in nanocomposite materials with dissipation effect. By considering the Kirchhoff plate theory and Kelvin–Voigt model, the governing equation is derived using Hamilton's principle. The equation is solved analytically to obtain the complex natural frequency. The parametric study is thoroughly performed, concentrating on the series effects of viscoelastic damping structure, aspect ratio, visco-Pasternak medium, and mode number. In this system, in-phase (IPV) and out-of-phase (OPV) vibrations are investigated. The numerical results of this article show a perfect correspondence with those of the previous researches.     

超音速流中二维板的Hopf分叉

应用Hamilton变分原理建立了对边简支对边自由薄板在超音速流作用下的非线性动力学方程,其中几何非线性采用Von-Kaman几何非线性关系进行描述,气动力采用了活塞理论。然后用Galerkin方法将偏微分方程化为常微分方程,并利用Hopf分叉的代数判据得到了系统临界流速随初始载荷变化的表达式以及颤振频率随初始载荷与临界流速变化的表达式,最后用数值方法进行了验证。     

计及结构阻尼的等截面梁纯弯曲振动的非线性分析

针对考虑挠度微分方程中高阶项所引起的几何非线性及材料阻尼所引起的阻尼非线性的梁，建立了梁纯弯曲振动时的非线性运动方程。利用非线性理论对该非线性问题进行了研究，得到了周期解稳定和不稳定区域的分界线方程和频率响应方程，得到忽略梁非线性因素的条件，得到了梁挠度微分方程中高阶项所引起的几何非线性项具有软特性效应等四点结论。     

低频大摆幅基础运动对滑动轴承-转子系统动力学特性的影响

考虑了低频大摆幅基础运动及转子在轴瓦内倾斜而产生的非线性油膜力矩等因素,基于拉格朗日方程建立了滑动轴承-转子系统的动力学模型。采用数值方法研究了基础运动对该系统非线性动力学特性的影响。结果表明:转子系统第一次失稳后其动力学分岔特性出现复杂的上下两支拟周期运动,并且第二次出现失稳的转速有所提高;在转子转速较高时,转子的振幅急剧增大,且在拟周期阶段就已经碰触轴瓦内壁而未能过渡到混沌状态。最后讨论了基础运动的摆动频率和幅值变化对系统动力学特性的影响。上述结论有助于认识低频大摆幅基础运动下滑动轴承-转子系统的运动规律。     

Vibrations of non-uniform functionally graded MWCNTs-polystyrene nanocomposite beams under action of moving load

Free and forced vibrations of non-uniform functionally graded multi-walled carbon nanotubes (MWCNTs)-polystyrene nanocomposite beams are investigated via Timoshenko beam theory. Different MWCNTs distributions in the thickness direction are introduced to improve fundamental natural frequency and dynamic behavior of non-uniform polymer composite beam under action of moving load. So, linear distribution patterns of carbon nanotubes (CNTs) in the thickness direction which can readily be achieved in practice are studied. The effects of shear deformation, rotary inertia, non-uniformity of the cross-section are also considered in the formulation. The finite element method is employed to obtain a numerical approximation of the motion equation. The non-uniform beam is approximated by another beam consisting of n elements with piecewise constant thickness so that the volume remains constant for each element. The effects of non-uniformity parameters, material distributions, velocity of the moving load and boundary conditions on the dynamic behavior are investigated. It is found that the symmetrical linear distribution of MWCNTs results in an increase in the fundamental natural frequency of nanocomposite beams which are higher than those of beams with uniform and unsymmetrical MWCNTs distributions.     

Nonlinear flow-induced vibration of a SWCNT with a geometrical imperfection

Based on the nonlocal continuum theory, transverse vibration of a single-walled carbon nanotube (SWCNT) conveying fluid with immovable support conditions is investigated. Unlike previous similar studies, the SWCNT is assumed to be not perfectly straight and initially includes a slight geometrical curvature as an imperfection. The SWCNT is assumed to be embedded in a Pasternak-type foundation. Hamilton’s principle is applied to drive an efficient governing equation of motion, which covers stretching, large deformation, and imperfection nonlinearities. The perturbation method of multi scales (MMS) is applied and the nonlinear flow-induced frequency ratio is analytically calculated. The obtained results reveal that the imperfection of the nanotube at high flow velocities makes the model severely nonlinear, especially when considering the nonlocal effects. A noteworthy observation is that the nonlinear flow-induced frequency ratio is decreased as the imperfection of the nanotube increases. Whereas through a parametric study, the effects of the flow velocity, nonlocal parameter, the stiffness of the elastic foundation, and the boundary conditions (BCs) on this frequency reduction are calculated and discussed widely.     

结构参数对机翼非线性颤振系统混沌运动特性的影响

机翼非线性颤振系统中的混沌运动是一种复杂的非线性动力学现象,研究结构参数对机翼非线性颤振系统混沌运动特性的影响,对非线性动力学系统的混沌运动控制具有重要意义。建立具有立方型非线性操纵刚度的带操纵面二元机翼的颤振方程,采用数值积分方法分别获得该非线性颤振系统在不同阻尼水平和不同操纵刚度下的分岔特性图。对分岔特性图进行对比分析结果表明：操纵面的操纵刚度并不影响系统的混沌运动特性,而操纵面偏转自由度或机翼俯仰自由度上的阻尼将会影响系统混沌颤振区域内的周期窗口,进而影响系统的混沌运动特性,特别是两自由度中任意一个的阻尼水平减小到一定程度时,系统混沌颤振区域内的周期窗口都将会消失;但是,单一的减小某个自由度上的阻尼水平,会使机翼非线性颤振系统的颤振临界速度降低。为了使得该系统在混沌颤振区域内不产生周期窗口又不降低其颤振临界速度,可采用在减小俯仰自由度阻尼的同时增大操纵面偏转自由度阻尼的方法。     

基于Bessel和Meijer-G函数的楔形和锥形悬臂梁振动分析

基于欧拉-伯努利梁理论,利用Lagrange法建立了楔形和锥形截面梁在外激作用下的非线性微分方程.提出了一种基于Bessel函数和Meijer-G函数线性组合的无需迭代及近似截断的振型函数,且该振型函数不依赖于楔形和锥形变截面梁的弯曲振动的运动方程是否为标准的Bessel形式,该方法能快速求解线性基频和模态函数.随后将...     

Noise-induced parametric oscillations in nonlinear oscillator

The onset of stochastic oscillations in a nonlinear oscillator with a noise-modulated frequency is considered. It is demonstrated that these oscillations are characterized by the existence of an attractor (i.e., are independent of the initial conditions), but do not exhibit the phenomenon of synchronization typical of self-oscillatory systems.     

Analysis of large amplitude free vibrations of unsymmetrically laminated composite beams on a nonlinear elastic foundation

The large amplitude free vibration of an unsymmetrically laminated composite beam (LCB) on a nonlinear elastic foundation subjected to axial load has been studied. The equation of motion for the axial and transverse deformations of a geometrically nonlinear LCB is derived. Using the Ritz method, the governing equation is reduced to a time-dependent Duffing equation with quadratic and cubic nonlinearities. The homotopy analysis method (HAM) is used to obtain exact expressions for the dynamic response of the LCB. This study shows that the third-order approximation of the HAM leads to highly accurate solutions that are valid for a wide range of vibration amplitudes. The effects of different parameters on the ratio of nonlinear to linear natural frequency of beams and the post-buckling load-deflection relationship are studied.     

Influence of in-plane pre-load on the vibration frequency of circular graphene sheet via nonlocal continuum theory

In this study, the free vibration behavior of circular graphene sheet under in-plane pre-load is studied. By using the nonlocal elasticity theory and Kirchhoff plate theory, the governing equation is derived for single-layered graphene sheets (SLGSs). The closed-form solution for frequency vibration of circular graphene sheets under in-plane pre-load has been obtained and nonlocal parameter appears into arguments of Bessel functions. The results are subsequently compared with valid result reported in the literature. The effects of the small scale, pre-load, mode number and boundary conditions on natural frequencies are investigated. The results are shown that at smaller radius of circular nanoplate, the effect of in-plane pre-loads is more importance.     

经典式Spar平台垂荡-纵摇耦合混沌运动研究

该文基于Lyapunov指数研究经典式Spar平台主体垂荡-纵摇非线性耦合的混沌运动。建立了规则波浪中平台主体垂荡-纵摇耦合非线性微分方程,以经典式Spar平台为例,数值计算了响应的最大Lyapunov指数谱及分岔图,在波高和波浪频率构成的平面上,计算了平台不稳定纵摇运动的参数域。结果表明,平台运动形式对波浪激励频率非常敏感,随着波浪频率的改变,Spar平台发生1/2亚谐运动、概周期运动,当波浪频率接近垂荡固有频率时,发生混沌运动。     

混凝土单桩在轴向扰力作用下的混沌运动

在考虑混凝土非线性本构关系的基础上,建立了混凝土单桩纵向振动的非线性动力方程。经研究发现本构关系为非线性的结构,在轴向扰动作用下其纵向振动也可能发生混沌运动。同时,讨论分析了扰力频率对结构发生混沌运动区域的影响。     

Analytical geometrical responses in large deflection of simply supported piezoelectric layered plate under initial tension

Abstract

The analytical geometrical responses in large deflection of a simply supported and layered piezoelectric circular plate under initial tension due to lateral pressure are presented. The approach follows von Karman plate theory for large deflection with a consideration of a symmetrically laminated case including a piezoelectric layer. The related nonlinear governing equations are derived in a non‐dimensional form and are simplified by neglecting the arising nonlinear terms, yielding a modified Bessel equation or a standard Bessel equation for the lateral slope. The associated analytical solutions are developed by imposing the simply supported edge conditions of the problem. For a 3‐layered nearly monolithic plate under a low pretension and a low applied voltage upon the piezoelectric layer, the results agree well with those obtained by using the classical plate theory for a single‐layered plate under pure mechanical loading, and thus the developed approach is validated. Typical 3‐layered piezoelectric plates are then implemented and the results show that, no apparent edge effect was found for the present problem. In additions, a piezoelectric effect appears to be present only up to a moderate initial tension. For a relatively high pretension, the tension effect tends to be dominant, resulting in nearly the same results for the geometrical responses, regardless of the magnitude of the applied voltage.     

水平地震激发的等截面立柱的非线性动力响应

本文采用非线性Ｒｎｙｌｅｉｇｈ阻尼来描述立柱在地震响应初期有激发而加速运动,至最大速度后开始衰减至停止运动,取适合所有边界条件的振型函数代入由非线性偏微分方程构成的控制方程,当立柱两端铰支时,其振型函数的系数为时间自变量的函数构成的富氏级数,应用富氏级数的正交性,此控制方程化为一无穷非线性常微分方程组,用逐次渐近法求解即每次只取一个未知函数,得到一个非齐次ＶａｎｄｅｒＰｏｌ方程,从而给出其头两次的渐近解,并给出其数值结果和讨论了解的分岔的意义。