液体三维晃动特征问题的有限元数值计算方法

本文采用有限元方法数值求解任意刚性容器内液体三维晃动的固有频率和模态。通过建立液体晃动特征问题的泛函极值原理，编制了四面体等参单元有限元程序，计算了平放圆柱腔内三维液体晃动的特征频率，并将矩形容器、球腔、带“十”字隔板球形容器内的液体三维晃动计算结果与解析解、实验结果和二维有限元数值解进行了比较，程序的正确性得到了验证。     

微重力环境下慢自旋充液容器内的液体晃动

本文研究在表面张力作用下自旋刚性容器内的部分充液液体的自由晃动问题。采用Pfeiffer方法建立了液体自由晃动特征值边值问题,利用边界元法数值求解晃动的特征频率和模态,分别计算给出球腔内的液体晃动关于充液比、微重Bond数和自旋Bond数的特征叛率曲线。     

任意三维贮箱内液体晃动的模态分析及其等效力学模型

本文采用有限元方法建立了数值求解任意三维贮箱内液体晃动固有频率和摸态、动力特征参数的通用程序，利用ANSYS有限元前处理模块．使得程序的通用性达到最大化。通过对液体受迫晃动的结果分析，发现了三维晃动中贮箱外激励与模态响应之间的复杂关系．并且提出了建立液体受迫晃动的等效力学模型的方法。本文以油罐车充液贮箱为例，数值研究了贮箱端部不同所引起的动力学差异，给出了晃动频率和晃动质量的变化曲线。     

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。     

任意轴对称腔充液系统的自旋稳定性

本文对具有任意轴对称腔的充液陀螺的永久转动给出了稳定性判据，该判据了考虑了腔内液体的晃动，通过对液体晃动特征模态求解的有限元分析，得到涉及液体晃动的判据修正量仅仅与液面的几何形状有关，本文分别给出了液面为旋转抛物面，去底旋转抛物面和圆柱面的判据修正量计算公式，经过数值试验发现了相应的解析公式。     

俯仰激励下液体大幅晃动问题研究

主要研究俯仰激励下液体大幅晃动问题，将ALE(arbitrary Lagrange-Euler)运动学描述引入到Navier-Stokes方程中，推导了俯仰激励下液体大幅晃动数值模拟计算公式，并利用Galerkin加权余量法推导了有限元数值离散方程，采用ALE有限元方法对方形贮腔中的液体大幅晃动进行了数值模拟计算，对结果进行了比较分析，揭示了俯仰激励下液体大幅晃动问题的非线性现象。     

俯仰激励下三维液体大幅晃动问题研究

主要研究俯仰激励下三维液体大幅晃动问题,将任意Lagrange-Euler法 (arbitrary Lagrange-Euler, ALE)运动学描述引入到Navier-Stokes方程中,推导了俯仰激励下液体大幅晃 动数值模拟计算公式,并利用Galerkin加权余量法推导了有限元数值离散方程和分步有限 元计算格式,采用ALE分步有限元方法对圆筒形贮腔中的液体大幅晃动进行了数值模拟计 算. 得到了波高、晃动力及晃动力矩等晃动特性的时间变化历程,并对结果进行了分析,揭 示了俯仰激励下三维液体大幅晃动问题的非线性现象.     

微重力状态下旋转对称刚性容器中液体的晃动响应

在文[1]的基础上,本文进一步研究了微重力状态下旋转对称刚性容器中液体的晃动响应问题,导出了液体晃动响应的计算公式。最后,对圆柱形容器作了具体计算,并将计算结果与实验数据进行了比较。 在文[1]中,已给出了微重力状态下旋转对称刚性容器中液体的静正自由液面及固有晃动频率的计算方法,在此基础上,现进一步研究其动态响应问题。     

微重力场中液体在带隔板球腔内的晃动

本文讨论微重力场中带球面隔板的球腔内液体晃动问题。选择Legendre函数作为Ritz方法的基函数,计算液体的自由晃动及腔体横向振动激励的受迫振动。计算结果表明,自由晃动频率随隔板位置的下降而趋于升高。液体晃动的动力学效应可用等效的质量—弹簧系统模拟。     

微重条件下两底为半球面腰为圆柱面的贮箱中液体的晃动特性

本文研究了微重条件下两底为半球面腰为圆柱面的贮箱中液体的晃动特性。首先分析了静液面形状。然后用一类特征函数展开的方法求出液体自由振动频率、液体对腔壁的反作用力和力矩,在此基础上得到了等效力学模型.最后给出了数值计算结果。     

Modal part analysis of slosh of the liquid in a cylindrical container in the case of small bond number

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Slosh dynamics of inviscid fluids in two‐dimensional tanks of various geometry using finite element method

This paper brings into focus some of the interesting effects arising from the motion of the liquid free surface due to sloshing in partially filled containers of several geometrical shapes in two dimensions. The slosh characteristics that include frequencies, free surface profiles and the hydrodynamic pressure over the container walls have been reported in this study. The equations of motion of the fluid, considered inviscid, are expressed in terms of the pressure variable alone. It is assumed that the frequency of the exciting oscillation is not in the immediate neighborhood of the natural slosh frequency, so that the slope of the free surface is small. Simple harmonic oscillation and earthquake excitations are used as the prescribed boundary conditions. A finite difference‐based iterative time‐stepping technique is employed to advance the solution in the time domain. The paper presents numerical solutions for rectangular, vertically mounted annular cylindrical, trapezoidal and horizontal circular cylindrical containers. Numerical results obtained are compared with the available existing solutions to validate the code developed. The parametric study of the slosh dynamic systems shows the importance of the nature of excitation, fluid height and the geometry of the container. Copyright © 2007 John Wiley & Sons, Ltd.     

自旋液体晃动研究

对旋转对称中心贮箱内的自旋液体晃动问题，提出了一个直接对Ｅｕｌｅｒ方程进行Ｇａｌｅｒｋｉｎ离散的近似方法，并分析了方法的近似性。     

液体晃动等效力学模型的参数识别

本文研究确定贮箱内液体晃动等效力学模型的参数的试验方法。通过对充液贮箱试验系统的简化分析得到系统的传递函数表达式,应用频响函数拟合方法得到了模型参数,在曲线拟合过程中利用权函数解决液体晃动的非线性影响因素。应用本文所述方法研究了某型号卫星推进剂贮箱的液体晃动问题。     

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     

Attitude tracking control of flexible spacecraft with large amplitude slosh

This paper is focused on attitude tracking control of a spacecraft that is equipped with flexible appendage and partially filled liquid propellant tank. The large amplitude liquid slosh is included by using a moving pulsating ball model that is further improved to estimate the settling location of liquid in microgravity or a zero-g environment. The flexible appendage is modelled as a three-dimensional Bernoulli–Euler beam, and the assumed modal method is employed.A hybrid controller that combines sliding mode control with an adaptive algorithm is designed for spacecraft to perform attitude tracking. The proposed controller has proved to be asymptotically stable. A nonlinear model for the overall coupled system including spacecraft attitude dynamics,liquid slosh, structural vibration and control action is established. Numerical simulation results are presented to show the dynamic behaviors of the coupled system and to verify the effectiveness of the control approach when the spacecraft undergoes the disturbance produced by large amplitude slosh and appendage vibration. Lastly, the designed adaptive algorithm is found to be effective to improve the precision of attitude tracking.     

Sloshing dynamics modulated cryogenic helium fluids driven by gravity gradient or jitter accelerations associated with slew motion in microgravity

The mathematical formulation of the Dewar container sloshing dynamics for a partially filled liquid of cryogenic superfluid helium II driven by the gravity gradient or jitter accelerations associated with slew motion in a microgravity environment are studied. The numerical computation of sloshing dynamics is based on the non-inertia container bounded frame and the solution of time-dependent, three-dimensional partial differential equations subjected to the initial and boundary conditions. This study discloses that the capillary effect of sloshing dynamics governs the liquid-vapor interface fluctuations driven by the gravity gradient or jitter accelerations associated with slew motion in a microgravity environment. The peculiar behavior of superfluid helium in response to sloshing dynamics is also investigated.     

Motion of a magnetizable liquid in a rotating magnetic field

Moskowitz and Rosensweig [1] describe the drag of a magnetic liquid — a colloidal suspension of ferromagnetic single-domain particles in a liquid carrier — by a rotating magnetic field. Various hydrodynamic models have been proposed [2, 3] to describe the macroscopic behavior of magnetic suspensions. In the model constructed in [2] it was assumed that the intensity of magnetization is always directed along the field so that the body torque is zero. Therefore, this model cannot account for the phenomenon under consideration. We make a number of simplifying assumptions to discuss the steady laminar flow of an incompressible viscous magnetizable liquid with internal rotation of particles moving in an infinitely long cylindrical container in a rotating magnetic field. The physical mechanism setting the liquid in motion is discussed. The importance of unsymmetric stresses and the phenomenon of relaxation of magnetization are emphasized. The solution obtained below is also a solution of the problem of the rotation of a polarizable liquid in a rotating electric field according to the model in [3].Translated from Zhurnal Prikladnoi Mekhaniki i Tekhnicheskoi Fiziki, No. 4, pp. 40–43, July–August, 1970.