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1.
在建立进动充液圆筒内液体偏差流动方程的基础上,结合液体惯性波和轴向二次流动线性解,通过对定常二次流动的线性稳定性分析,提出了函数空间表达的流动不稳定性非线性分岔分析方程. 对非惯性坐标系下液体流动的Navier-Stokes方程进行了数值求解,并对惯性波发生破裂(实验提供的3种主模态下得出的共振破裂现象)时的压力时间序列进行分析,得出了液体流动不稳定的基本非线性特征.  相似文献   

2.
Nonlinear vibration of circular sandwich plate under the uniformed load   总被引:3,自引:1,他引:2  
IntroductionSofar,onlyafewpeoplehavestudiedthelargedeflectionproblemsofsandwichplatesandshellsbecauseofthedifficultyofnonlinearmathematics.LiuRenhuaihasdonemuchtofindaseriesofresultswiththevalueofapplicationinengineeringpractice[1~5].Author[6,7]hadtheiniti…  相似文献   

3.
Non-linear coupled vertical and torsional vibrations of suspension bridges are investigated. Method of Multiple Scales, a perturbation technique, is applied to the equations to find approximate analytical solutions. The equations are not discretized as usually done, rather the perturbation method is applied directly to the partial differential equations. Free and forced vibrations with damping are investigated in detail. Amplitude and phase modulation equations are obtained. The dependence of non-linear frequency on amplitude is described. Steady-state solutions are analyzed. Frequency-response equation is derived and the jump phenomenon in the frequency-response curves resulting from non-linearity is considered. Effects of initial amplitude and phase values, amplitude of excitation, and damping coefficient on modal amplitudes, are determined.  相似文献   

4.
静载荷作用下柔韧圆板的大幅度振动   总被引:2,自引:1,他引:2  
本文首先给出了均布载荷作用下柔韧圆板的大幅度振动方程,按文中给出的时间模态假设导了该问题的非线性耦合的代数和微分特征方程组,利用修正迭代法求出了该方程组的近似解析解,得到了柔韧圆振动的幅频-载荷特征关系,讨论了静载荷对其振动性态的影响。  相似文献   

5.
冲击动力系统的鲁棒稳定性分析   总被引:3,自引:0,他引:3  
考虑冲击动力系统的k-p周期运动的鲁棒稳定性问题。首先,根据微分方程的解、冲击条件和衔接条件,应用迭代法给出了系统存在k-p周期运动的充分必要条件,并利用稳定性的等价原理,通过周期运动的扰动差分方程导出其稳定条件;然后,着重对含有不确定参数的冲击动力系统的k-p周期运动的稳定性进行了分析,得出了鲁棒稳定的充分条件,文末给出了用于阐明理论结果的算例。  相似文献   

6.
Sabatini  Luca  Augusti  Giuliano 《Meccanica》2000,35(6):519-546
The laws governing the propagation, growth and decay of acceleration waves in directed models of elastic beams are deduced for materials with zero and non-zero heat flux, that is non-conductors and conductors of heat. The equations depend explicitly on the geometric and inertial characteristic of the beam section and on the mechanical properties of the material. Solutions are derived for the velocities of propagation and the evolution (amplitude variation) of each type of wave (extension, bending, shear, twist). Results are discussed and some numerical examples presented.  相似文献   

7.
Governing equations of axisymmetric finite dynamic deformations of an incompressible, isotropic and elastic cylindrical shell made of Neo-Hookean materials are derived. The non-linear partial differential equations are simplified for the cases where all deformation variations along the thickness of the tube may be neglected. The simplified non-linear equations are then solved exactly to arrive at traveling wave solutions along the axis. These wave solutions are called controllable because they can be maintained by prescribable surface stresses, bounded amplitude and frequency of excitations alone.  相似文献   

8.
The nonlinear behavior of a cantilevered fluid conveying pipe subjected to principal parametric and internal resonances is investigated in this paper. The flow velocity is divided into constant and sinusoidai parts. The velocity value of the constant part is so adjusted such that the system exhibits 3:1 internal resonances for the first two modes. The method of multiple scales is employed to obtain the response of the system and a set of four first-order nonlinear ordinary-differential equations for governing the amplitude of the response. The eigenvalues of the Jacobian matrix are used to assess the stability of the equilibrium solutions with varying parameters. The codimension 2 derived from the double-zero eigenvaiues is analyzed in detail. The results show that the response amplitude may undergo saddle-node, pitchfork, Hopf, homoclinic loop and period-doubling bifurcations depending on the frequency and amplitude of the sinusoidal flow. When the frequency of the sinusoidal flow equals exactly half of the first-mode frequency, the system has a route to chaos by period-doubling bifurcation and then returns to a periodic motion as the amplitude of the sinusoidal flow increases.  相似文献   

9.
Periodic solutions for parametrically excited system under state feedback control with a time delay are investigated. Using the asymptotic perturbation method, two slow-flow equations for the amplitude and phase of the parametric resonance response are derived. Their fixed points correspond to limit cycles (phase-locked periodic solutions) for the starting system. In the system without control, periodic solutions (if any) exist only for fixed values of amplitude and phase and depend on the system parameters and excitation amplitude. In many cases, the amplitudes of periodic solutions do not correspond to the technical requirements. On the contrary, it is demonstrated that, if the vibration control terms are added, stable periodic solutions with arbitrarily chosen amplitude and phase can be accomplished. Therefore, an effective vibration control is possible if appropriate time delay and feedback gains are chosen.  相似文献   

10.
The non-linear non-planar steady-state responses of a near-square cantilevered beam (a special case of inextensional beams) with general imperfection under harmonic base excitation is investigated. By applying the combination of the multiple scales method and the Galerkin procedure to two non-linear integro-differential equations derived in part I, two modulation non-linear coupled first-order differential equations are obtained for the case of a primary resonance with a one-to-one internal resonance. The modulation equations contain linear imperfection-induced terms in addition to cubic geometric and inertial terms. Variations of the steady-state response amplitude curves with different parameters are presented. Bifurcation analyses of fixed points show that the influence of geometric imperfection on the steady-state responses can be significant to a great extent although the imperfection is small. The phenomenon of frequency island generation is also observed.  相似文献   

11.
胡宇达  张晓宇 《应用力学学报》2020,(2):674-681,I0015
研究了轴向运动正交各向异性条形薄板在线载荷作用下的超谐波共振问题。通过哈密顿原理导出了几何非线性下正交各向异性条形板的非线性振动方程。运用伽辽金积分法,推得了关于时间变量的量纲归一化非线性振动微分方程组。应用多尺度法求解三阶超谐波共振问题,得到了稳态运动下一阶、二阶、三阶共振形式的共振幅值响应方程。利用Liapunov方法推得不同共振形式稳态解的稳定性判据,并据此分析不同参数对系统稳定性的影响。绘制了振幅特性变化曲线图和与之对应的激发共振多解临界点曲线图,分析系统参数对共振的影响,并预测系统进入非线性共振区域的临界条件。得出激励在特定位置区间时可激发系统的超谐波共振,随着激励幅值的增加,上稳定解支减小,下稳定解支增加,且一阶模态振幅大于二阶、三阶振幅。  相似文献   

12.
A Rayleigh–Liénard oscillator excited by a fundamentalresonance is investigated by using an asymptotic perturbation method based on Fourier expansion and time rescaling. Two first-order nonlinear ordinarydifferential equations governing the modulation of the amplitude andthe phase of solutions are derived. These equations are used todetermine steady-state responses and their stability. Excitationamplitude-response and frequency-response curves are shown and checkedby numerical integration. Dulac's criterion, the Poincaré–Bendixsontheorem, and energy considerations are used in order to study the existenceand characteristics of limit cycles of the two modulation equations. Alimit cycle corresponds to a modulated motion for the Rayleigh–Liénardoscillator. For small excitation amplitude, the analytical results arein excellent agreement with the numerical solutions. In certain caseswhen the excitation amplitude is very low, an approximate analyticsolution corresponding to a modulated motion can be obtained andnumerically checked. Moreover, if the excitation amplitude is increased,an infinite-period bifurcation occurs because the modulation periodlengthens and becomes infinite, while the modulation amplitude remainsfinite and suddenly the attractor settles down into a periodic motion.  相似文献   

13.
The complex amplitude modulation equations of a discrete dynamicalsystem are derived under general conditions of simultaneous internal andexternal resonances. Alternative forms of the real amplitude and phaseequations are critically discussed. First, the most popular polar formis considered. Its properties, known in literature for a multitude ofspecific problems, are here proven for the general case. Moreover, thedrawbacks encountered in the stability analysis of incomplete motions(i.e. motions containing some zero amplitudes) are discussed as aconsequence of the fact the equations are not in standard normal form.Second, a so-called Cartesian rotating form is introduced, which makesit possible to evaluate periodic solutions and analyze their stability,even if they are incomplete. Although the rotating form calls for theenlargement of the space and is not amenable to analysis of transientmotions, it systematically justifies the change of variables sometimesused in literature to avoid the problems of the polar form. Third, amixed polar-Cartesian form is presented. Starting from the hypothesisthat there exists a suitable number of amplitudes which do not vanish inany motion, it is proved that the mixed form leads to standard formequations with the same dimension as the polar form. However, if suchprincipal amplitudes do not exist, more than one standard form equationshould be sought. Finally, some illustrative examples of the theory arepresented.  相似文献   

14.
In this paper, we obtain a third-order approximate solution for the laminar boundary layer between two planes perpendicular to each other.In boundary layer equations, the viscous and the inertial terms have the same quantity step. In this paper, at first, supposing that the inertial terms are bigger than the viscous terms, we solve the boundary layer equations, and then we suppose that the viscous terms are bigger than the inertial terms. At last, we take the mean value as the valid solution of the boundary layer equations.The first- and the second-order approximate solutions obtained in this paper coincide with the results in ref. [1], while the third-order solution obtained in this paper is better than that in ref. [1].  相似文献   

15.
Theory of nonlinear dynamic stability for composite laminated plates   总被引:2,自引:1,他引:1  
In this paper,the general equations of dynamic stability for composite laminatedplates are derived by Hamilton principle.These general equations can be used to considerthose different factors that affect the dynamic stability of laminated plates.The factors aretransverse shear deformation,initial imperfections,longitudinal and rotational inertia,andply-angle of the fiber,etc.The solutions of the fundamental equations show that someimportant characteristics of the dynamic instability can only be got by the considerationand analysis of those factors  相似文献   

16.
The aim of the present paper is to give a survey of those exact solutions of relativistic inertial navigation equations which are directly or indirectly related to Thomas precession. Various cases of uniform circular motion of an object in gravity-free space close to motion with inertial or orbital attitude are considered.  相似文献   

17.
The paper deals with theoretical problems of analysis of forced harmonic vibrations in liquid-saturated porous structures. The differential equations of motion written for the vector of the solid phase displacements and the liquid phase pressure are derived from the equations of phase component dynamics and the constitutive equations of anisotropic continuum. An example of transverse vibrations of a porous framing is used to study the influence of material constants on the dynamic characteristics of a poroelastic system. It is shown that an increase in the excitation frequency significantly increases the effect of inertial interaction between the phases of the poroelastic material, especially for the amplitudes of the liquid pressure in the pores. Thus, to obtain exact solutions of problems of poroelastic material dynamics, it is necessary to take into account all types of interaction between the solid and liquid phases of heterogenous materials.  相似文献   

18.
In the study of nonlinear vibrations of planar frames and beams with infinitesimal displacements and strains, the influence of the static displacements resulting from gravity effect and other conservative loads is usually disregarded. This paper discusses the effect of the deformed equilibrium configuration on the nonlinear vibrations through the analysis of two planar structures. Both structures present a two-to-one internal resonance and a primary response of the second mode. The equations of motion are reduced to two degrees of freedom and contain all geometrical and inertial nonlinear terms. These equations are derived by modal superposition with additional subsidiary conditions. In the two cases analyzed, the deformed equilibrium configuration virtually coincides with the undeformed configuration. Also, 2% is the maximum difference presented by the first two lower frequencies. The modes are practically coincident for the deformed and undeformed configurations. Nevertheless, the analysis of the frequency response curves clearly shows that the effect of the deformed equilibrium configuration produces a significant translation along the detuning factor axis. Such effect is even more important in the amplitude response curves. The phenomena represented by these curves may be distinct for the same excitation amplitude.  相似文献   

19.
The nonlinear dynamics of a clamped-clamped/sliding inextensional elastic beam subject to a harmonic axial load is investigated. The Galerkin method is used on the coupled bending-bending-torsional nonlinear equations with inertial and geometric nonlinearities and the resulting two second order ordinary differential equations are studied by the method of multiple time seales and by direct numerical integration. The amplitude equations are analyzed for steady and Hopf bifurcations. Depending on the amplitude of excitation, the damping and the ratio of principal flexural rigidities, various qualitatively distinct frequency response diagrams are uncovered and limit cycles and chaotic motions are found. In the truncated two-degree-of-freedom system the transition from periodic to chaotic amplitude-modulated motions is via the process of torus doubling and subsequent destruction of the torus.  相似文献   

20.
挠性联结双体航天器的稳定性与分岔   总被引:3,自引:0,他引:3  
刘延柱  成功 《力学学报》2000,32(2):207-212
研究圆轨道内受万有引力矩作用的挠性联结双体航天器在轨道平面内的姿态运动,讨论其相对轨道坐标系统平衡状态的稳定性与分岔。提出判平衡方程非平凡解存在性的几何方法,并应用Liapunov直接法、Liapunov-Schmidt约化方法和奇异性理论导出解析形式的稳定性与分岔的充要条件,从而对系统的全局运动性态作出定性的描述。  相似文献   

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