俯仰运动圆柱贮箱中液体的非线性晃动

首次对储仰运动圆柱贮箱中液体的有限幅值晃动问题进行了解析研究。首先建立了描述俯仰和／或偏航运动贮箱中液体晃动的非线性偏微分方程组,而后提出了相应的变分原理,建立了压力体积分形式的Ｌａｇｒａｎｇｅ函数,通过变分方程,最终得到措述俯仰和／或偏航运动圆柱贮箱中液体晃动的非线性动力学微分方程组,该动力学方程组自然满足液体自由表面的运动学和动力学办界条件。而后动用多尺度法求解了所得的动力学方程组,对非线性液     

低重环境下俯仰运动圆柱贮箱内液体晃动

考虑低重环境下由于表面张力的影响使得圆柱贮箱内液体呈现弯曲自由液面的情况,以俯仰激励下液体晃动的占优模态振型函数为晃动速度势的基函数,利用傅里叶-贝塞尔级数对贮箱受俯仰激励时的自由液面处的运动边界条件进行展开,得到能描述晃动系统本质的广义状态方程,并分别给出了固有频率、晃动波高、晃动力和晃动力矩等晃动特征的计算方法. 通过具体算例得到了俯仰激励下贮箱内液体晃动特征的动态响应,同时验证了文中方法的收敛性、可行性和正确性.      

DYNAMICAL CHARACTERISTICS ANALYSIS FOR UNILATERAL CONSTRAINED SIMPLY SUPPORTED BEAM WITH HARMONIC WAVE EXCITATION1)

为研究间隙碰撞对系统动力学响应的影响,以理想简支梁的振型函数为Rayleigh--Ritz基函数建立了单侧约束简支梁系统的非线性离散动力学方程组,应用数值方法研究了系统在基础谐波激励下的动力学响应特征及其对共振频率线性等效方法适用性的影响。研究表明：非线性动力学系统间隙产生的局部碰撞,使得系统振动能量在系统各阶模态之间转移,使得线性等效方法失效;即使进行非线性分析,也需要考虑系统固有频率远大于激励频段上限的模态。     

基于约束函数法的热力耦合有限元分析

分析了滑移接触条件下热力耦合现象,建立了热力耦合的有限元分析连续模型,提出了系统动力学平衡方程和热力学平衡方程。对系统中物体间的接触条件进行了分析,得到了物体间接触条件的数学表达式,在此基础上,用约束函数表示接触约束条件。应用变分原理对约束函数进行变分,与系统平衡方程组成非线性方程组对热力耦合问题进行求解。实例表明,用约束函数法求解热力耦合问题,收敛性较好,算法稳定,计算结果能反映实际。     

基础谐波激励单侧约束简支梁系统的动力学特征分析

为研究间隙碰撞对系统动力学响应的影响,以理想简支梁的振型函数为Rayleigh–Ritz基函数建立了单侧约束简支梁系统的非线性离散动力学方程组,应用数值方法研究了系统在基础谐波激励下的动力学响应特征及其对共振频率线性等效方法适用性的影响。研究表明:非线性动力学系统间隙产生的局部碰撞,使得系统振动能量在系统各阶模态之间转移,使得线性等效方法失效;即使进行非线性分析,也需要考虑系统固有频率远大于激励频段上限的模态。     

电磁场中载流薄板的弯曲行为分析

在建立载流薄板的非线性磁弹性运动方程、电动力学方程和Lorentz力表达式的基础上,通过变量代换,将描述薄板的磁弹性状态方程整理成含有10个基本函数的标准Cauchy型.采用差分法及准线性化方法,将标准Cauchy型非线性偏微分方程组,变换成为能够用离散正交法求解的准线性微分方程组.通过算例,得到了电磁场与机械载荷联合...     

复合柔性结构全局模态函数提取与状态空间模型构建

随着航空航天等领域中实际工程结构的大型化和柔性化,结构的非线性振动和主动振动控制问题越来越凸显.分析和处理此类结构出现的复杂振动问题的关键在于建立系统的非线性动力学模型与状态空间模型.对于由柔性部件、刚体、连接部件构成的复合柔性结构,由于各部件之间的振动耦合效应,单个柔性部件在悬臂、简支和自由等静定边界下的模态与结构的真实模态有较大差异.为此,本文提出复合柔性结构全局模态的解析提取方法,通过全局模态离散得到系统非线性动力学模型,从而构建状态空间模型.该方法采用笛卡尔坐标描述系统的运动,建立系统的运动方程;结合描述柔性部件的偏微分方程、刚体的常微分运动方程、连接界面处力、力矩、位移和转角的匹配条件以及系统的边界条件,利用分离变量法给出统一形式的频率方程,获取系统的固有频率和解析函数表征的全局模态.这里提出的全局模态提取方法不仅便于复合柔性结构固有频率和全局模态的参数化分析,而且为建立复合柔性结构低维非线性动力学模型和状态空间模型提供了有效的途径,对于推进这类结构的非线性动力学分析与主动振动控制研究具有重要意义.      

刚体撞水非线性响应的边界元分析

考虑了非线性性液面条件液面条件,采用边界元法,始终撞水物体和水看成一个耦合系统,并作为一个冲击／接触问题处理。在自由注面的处理上,采用逐步迭代方法,使其始终满足液面的非线性条件,最终使自由液面达到一满足非线性条件的稳定值。而在撞水力的求解上,亦采用与自由液面相关的逐步迭代逼近方法,求取其稳定值。文中最后给出了几种不同情况下二维圆柱刚体撞水的计算实例,结果有力表明记叙虎法的可靠性和有效性。     

大气运动不稳定的变分原理(Ⅰ)

本文利用非线性基本方程组和变分原理研究旋转大气运动的不稳定性问题。文中所用方法是普遍适用的,对各种可能的基流模型都可获得其不稳定性判据。例如:适合于正压或斜压、分层或连续模型以及准地转模式或原始方程组;基流可以是带状或非带状的(即平行流或非平行流),定常的或非定常的。 虽然基流具有多样性,但它们在由相应的不变泛函所决定的空间内都是驻点(临界点)。如果在相应的泛函中将角动量守恒包括进去,那么基流可以是非定常流。 无论线性或非线性二阶变分都给出不稳定性判据。但尤其值得一提的是,本文第一次得到关于非定常基流,地形扰动流和非地转流的不稳定性判据。 同时本文也指出了线性理论和我们发展的变分原理所得到的不稳定性判据之间的差别,该差别说明用非线性基本方程组的重要性。 在最后一节,将该理论推广到流体不具有有限能量,因而变分原理不能直接应用的情况,如卢平面,然而广义的Liapounoff函数仍然可以在变分考虑下得到。      

圆筒形贮腔中微重力液体非线性晃动的数值模拟

本文讨论低重力液体在圆筒形贮腔中的非线性晃动问题。将ALE（任意的拉格朗日－欧拉）运动学描述关系引入到Navier-Stokes方程中,在时间域上采用分步离散方法中的速度修正格式,利用Galerkinlk加权余量方法推导了系统的有限元数值离散方程;推导了考虑表面张力效应时有限元边界条件的弱积分形式。推导了自由液面上法向矢量的计算公式。模拟了圆筒形贮腔中低重力液体的非线性晃动,并得到了自由液面、波高变化、压力响应等非线性动力特性。揭示了微重力液体非线性晃动的重要特征并将所得结论与现有的实验结果进行了比较。从而证实了本文方法的有效性与正确性。     

Stable response of low-gravity liquid non-linear sloshing in a circle cylindrical tank

Under pitch excitation,the sloshing of liquid in circular cylindrical tank includes planar motion,rotary motion and rotary motion inside planar motion.The boundaries between stable motion and unstable motion depend on the radius of the tank,the liquid height,the gravitational intension,the surface tensor and the sloshing damping.In this article,the differential equations of nonlinear sloshing are built first. And by variational principle,the Lagrange function of liquid pressure is constructed in volume intergration form.Then the velocity potential function is expanded in series by wave height function at the free surface.The nonlinear equations with kinematics and dynamics free surface boundary conditions through variation are derived.At last,these equations are solved by multiple-scales method.The influence of Bond number on the global stable response of nonlinear liquid sloshing in circular cylinder tank is analyzed in detail.The result indicates that variation of amplitude frequency response characteristics of the system with Bond,jump,lag and other nonlinear phenomena of liquid sloshing are investigated.     

Mathematical modelling and control of a nonholonomic spherical robot on a variable-slope inclined plane using terminal sliding mode control

In this paper, the three degrees-of-freedom motion of a two-dimensional rectangular liquid tank under wave action is simulated by the boundary element method in time domain. The coupling effects between tank motion and internal sloshing flow are investigated in partially filled conditions. The fourth-order Runge–Kutta method is adopted to update the wave shape and velocity potential on the free surface. The fully nonlinear mutual dependence of the incident wave, tank motion and internal sloshing flow is decoupled through an auxiliary function method, by which the liquid tank acceleration can be obtained directly without knowing the pressure distribution. The corresponding validation of numerical model is carried out and indicates that the accuracy of the present method is satisfactory to evaluate the dynamic responses of tank and sloshing motion. The corresponding response amplitude operators of tank motions for various wave frequencies, amplitudes and filling conditions are obtained, and the nonlinear coupling effects of sloshing flow on the tank responses are analyzed. It is found that the coupling effects have significant influence on sway and roll motion while have little impact on heave motion. The most important coupling effects on roll motion are the split of peak. In addition, due to the nonlinearity of sloshing flow, the roll motion amplitude is not linearly proportional to wave amplitude.     

Multidimensional modal analysis of liquid nonlinear sloshing in right circular cylindrical tank

The multidimensional modal theory proposed by Faltinsen,et al.(2000) is applied to solve liquid nonlinear free sloshing in right circular cylindrical tank for the first time. After selecting the leading modes and fixing the order of magnitudes baaed on the Narimanov-Moiseev third order asymptotic hypothesis,the general infinite dimensional modal system is reduced to a five dimensional asymptotic modal system (the system of second order nonlinear ordinary differential equations coupling the generalized time dependent coordinates of free surface wave elevation).The numerical integrations of this modal system discover most important nonlinear phenomena,which agree well with both pervious analytic theories and experimental observations. The results indicate that the multidimensional modal method is a very good tool for solving liquid nonlinear sloshing dynamics and will be developed to investigate more complex sloshing problem in our following work.     

多储液腔航天器刚液耦合动力学与复合控制

采用复合控制方法对充液航天器的姿态和轨道机动进行高精度控制.通过傅里叶-贝塞尔级数展开法,将低重力环境下液体的弯曲自由表面的动态边界条件转化为简单的微分方程,其中耦合液体晃动方程的状态向量由相对势函数的模态坐标和波高的模态坐标组成.通过广义准坐标下的拉格朗日方程得到航天器刚体部分运动和液体燃料晃动的耦合动力学方程,提出了自适应快速终端滑模策略和输入整形技术相结合的复合控制器,并分别用于控制携带有一个燃料腔和四个燃料腔航天器的轨道机动和姿态机动.通过数值模拟来验证控制器的效率和精度.结果表明,对于多储液腔航天器,如果在设计航天器的姿态和轨道控制器时没有充分考虑燃料晃动效应,那么在受控航天器系统中将会出现刚-液-控耦合问题并导致航天器姿态不稳定.而本研究中的复合自适应终端滑模控制器可以实现航天器机动的高精度控制并有效抑制液体燃料晃动.     

微重力下圆柱形贮箱内液体晃动的分岔现象

为了得到微重力下液体晃动的特性,晃动模态用具有水平静液面的液体晃动模态近似. 液体晃动取前5 个重要模态,用Lagrange 方程推导了横向力作用下液体晃动和航天器结构的无量纲的耦合动力学方程并进行数值模拟. 模拟了液体晃动模态随外力振幅和频率变化产生的分岔现象,并分析了系统参数,如Bond数、接触角、接触角迟滞、充液高度、频率比、质量比以及外力的周期形式和方向等对晃动模态的分岔的影响.     

Non-linear multimodal model for tuned liquid dampers of arbitrary tank geometry

Tuned liquid dampers (TLDs) utilize sloshing fluid to absorb and dissipate structural vibrational energy. Simple TLD tank geometries may not always be feasible due to space limitations. While the non-linear modelling of sloshing fluid is currently limited to tanks of simple geometries, this paper develops a non-linear multimodal model which describes the sloshing behaviour of a fluid in a flat-bottom tank of arbitrary geometry. The mode shapes of the sloshing fluid are found by solving the Helmholtz equation over the tank domain using the finite element method. The Bateman-Luke variational principle is used to develop a system of ordinary differential equations which account for the coupling of the sloshing modes through the non-linear free surface boundary conditions. Damping is incorporated into the model by considering the drag produced on a set of damping screens inserted in the fluid. The system of ordinary differential equations is solved using the Runge-Kutta-Gill Method to predict the wave heights and sloshing forces. In general, the mode shapes in an arbitrary tank will have components in two orthogonal (x- and y-) directions. This out-of-plane behaviour is an important consideration for TLD design. The model is validated with existing models for the special cases of rectangular and circular tanks. Lastly, new shake table tests are conducted on a tank of complex geometry.     

三维液体非线性晃动动力学特性的数值模拟

主要讨论圆筒形贮腔中三维液体非线性晃动问题,将任意的拉格朗日-欧拉（即ArbitraryLagrangian-Eulerian,简称ALE）运动学描述引入到Navies-Stokes方程中,在时间域上采用一种速度和压力的分步计算格式进行时间离散;在空间域上利用Galerkin加权余量法对系统方程进行数值离散;得到了数值计算粘性不可压液体非线性晃动的ALE分步有限元法的计算格式,推导了三维液体自由液面上结点法向矢量的数值计算方法,模拟了圆筒形贮腔（包括带圆环形隔板的圆筒形贮腔）中三维液体的非线性晃动;并得到了一些重要的非线必不知所云 性,通过数值模拟结果与实验结果的比较,证明实了本文方法的可靠性与有效性。     

Nonlinear simulation of a tuned liquid damper with damping screens using a modal expansion technique

Tuned liquid dampers utilize sloshing fluid to control wind-induced structural motions. However, as a result of the nonlinear free surface boundary conditions of fluid sloshing in a two-dimensional rectangular container, a closed-form solution describing the response behaviour is unavailable. Modal expansions, which couple the sloshing modes, are carried out to the first, third and fifth order to construct a system of coupled nonlinear ordinary differential equations that are solved using the Runge–Kutta–Gill Method. Modal damping is incorporated to account for energy losses arising from the fluid viscosity and the inclusion of damping screens. The model is in general agreement with a previous third-order model that incorporated screen damping in the fundamental sloshing mode only. Sinusoidal shake table experiments are conducted to validate the proposed models. Response time histories and frequency response plots assess the model’s prediction of wave heights, sloshing forces, and screen forces. The first-order model accurately predicts the resonant sloshing forces, and forces on a mid-tank screen. The higher-order models better represent the wave heights and forces on an off-centre screen. Experimental results from structure–TLD system tests under random excitation are used to evaluate the performance of the proposed models. The first-order model is able to predict the variance of the structural response and the effective damping the TLD adds to the structure, but as a minimum, a third-order model should be employed to predict the fluid response. It is concluded that a first-order model can be utilized for preliminary TLD design, while a higher-order model should be used to determine the required tank freeboard and the loading on damping screens positioned at off-centre locations.