球壳结构馈通增长的瑞利-泰勒不稳定性

利用小扰动分析法 ,导出不可压缩球壳结构的馈通增长方程 ,数值模拟了高压气体驱动外表面有初始扰动的明胶球壳的瑞利 泰勒不稳定性模型。计算结果表明 :对于低波数扰动 ,外界面比较稳定 ,内表面的馈通增长较快 ,具有比较明显的三个演化阶段和波形反转现象。高波数扰动的增长恰好与低波数相反。球壳会聚结构比柱壳会聚结构的界面稳定性要好些。     

改进的物理融合神经网络在瑞利?泰勒不稳定性问题中的应用

基于相场法的物理融合神经网络PF-PINNs被成功用于两相流动的建模, 为两相流动的高精度直接数值模拟提供了全新的技术手段. 相场法作为一种新兴的界面捕捉方法, 其引入确保了界面的质量守恒, 显著提高了相界面的捕捉精度; 但是相场法中高阶导数的存在也降低了神经网络的训练速度. 为了提升计算训练过程的效率, 本文在PF-PINNS框架下, 参考深度混合残差方法MIM, 将化学能作为辅助变量以及神经网络的输出之一, 并修改了物理约束项的形式, 使辅助变量与相分数的关系式由硬约束转为了软约束. 上述两点改进显著降低了自动微分过程中计算图的规模, 节约了求导过程中的计算开销. 同时, 为了评估建立的PF-PINNS在雷诺数较高、计算量较大的场景中的建模能力, 本文将瑞利?泰勒RT不稳定性问题作为验证算例. 与高精度谱元法的定性与定量对比结果表明, 改进PF-PINNs有能力捕捉到两相界面的强非线性演化过程, 且计算精度接近传统算法, 计算结果符合物理规律. 改进前后的对比结果表明, 深度混合残差方法能够显著降低PF-PINNS的训练用时. 本文所述方法是进一步提升神经网络训练速度的重要参考资料, 并为探索高精度智能建模方法提供了全新的见解.      

一类刚-柔耦合系统的建模与稳定性研究

对于由中心刚体带有柔性梁附件组成的这一类简单刚 柔耦合系统，目前文献广泛采用的Ｅｕｌｅｒ Ｂｅｒｎｏｕｌｉ梁模型中考虑的刚 柔运动耦合项有严重的缺陷．本文对于物理本构关系线性的有限变形梁，分别采用微元法和变分法建立了该系统大挠度非线性动力学方程组．本文使用严格的方法来研究此非线性耦合动力学模型，采用能量 动量矩组合方法构成Ｌｉａｐｕｎｏｖ函数，严格证明了此非线性系统平凡解的积分范数稳定性以及具有鲜明物理意义的最大模范数稳定性．本文对文献中引用的三类线性化模型，采用假设模态法，对中心刚体匀速转动时梁的振动作了数值仿真，进一步验证了本文的结论．上述结果，对选择刚 柔耦合系统正确的动力学模型是有益的．     

结构模态耦合试验稳定性裕度研究及应用

针对某型验证机纵向伺服弹性稳定性裕度不足的问题,建立了基于结构模态耦合试验和仿真的分析方法。通过比较原型机与验证机之间传感器幅值裕度和响应曲线,初步判定传感器安装结构响应过大为此次裕度不足的主要原因。通过控制律仿真环节和机体动力学仿真环节建立了结构模态耦合仿真模型,模拟试验输入信号,获得传感器响应数据。通过结构模态耦合仿真,验证了倍频现象是导致传感器安装结构响应过大的原因,进而导致纵向稳定性裕度不足。提出了一种传感器支持系统可调频率动态控制装置,可有效提升结构模态耦合试验稳定性裕度。

     

一类刚-梁耦合系统平面稳态运动的稳定性

研究了中心力场中的一类刚-弹耦合系统的平面运动动力学，模型是带有一悬臂 梁的刚体. 综合考虑了系统轨道运动与姿态运动，在Lagrange力学体系下给出了系统的运 动方程，在保守系统和考虑梁的材料黏滞阻尼两种情况下，利用能量-动量方法给出了一类 相对平衡点稳定性的充分条件.     

一类刚-梁耦合系统定态运动的稳定性

采用带有一悬臂梁的刚体模型, 研究了一类自由的刚-弹耦合系统定态运动的稳定 性. 直接从原始系统出发(未做离散化处理),综合考虑了系统的平动与姿态运动的 耦合,在非完整坐标的Lagrange力学体系下选取状态变量,结合Lyapunov直接方 法和Chetaev的从运动方程的首次积分构造Lyapunov泛函的 方法. 引入的变量使得Lyapunov泛函形式简单,给运动稳定性分析带来了很大的方便. 最终给出了系统的定态运动按尺度稳定的充分条件.     

流体-结构耦合问题的有限元并行计算研究

流体-结构耦合问题广泛存在于各种工程领域,本文采用ALE显式有限元法求解该类问题,并对该方法的并行性进行讨论。同时根据流体-结构耦合问题与ALE显式有限元的计算特点,在坐标递归分区方法的基础上设计并程序实现了基于流体-结构耦合均衡的分区算法。通过与坐标递归分区方法的计算结果相比较,对于流体-结构耦合问题的求解,耦合均衡并行分区方法具有更好的加速比和并行效率。     

可压缩性对Rayleigh-Taylor不稳定性的影响

对于状态方程为压力是密度的任意单值函数的理想流体 ,导出了Rayleigh Taylor不稳定性色散关系的一般形式。它表明 :较重流体易压缩是稳定因素 ,较轻流体易压缩是不稳定因素。可压缩性在重力场作用下形成的密度分布是稳定性因素 ,而膨胀压缩效应是不稳定因素。     

流体可压缩性对Rayleigh-Taylor不稳定性影响机理分析

在等熵方程为压力是密度的任意单值函数形式情况下 ,分析了R T(Rayleigh Taylor)不稳定性中流体可压缩性的作用。在没有边界效应的条件下所作的分析表明 :在重力场作用下流体可压缩性形成的密度分布是R T不稳定性中的致稳因素 ,而扰动流体的膨胀 (收缩 )效应助长R T不稳定性的发展 ;上层重流体的可压缩性是稳定因素 ,而下层轻流体的可压缩性是失稳因素。从扰动发展驱动力和扰动带动的等效质量两个方面对该结论的物理机制进行了分析。     

高Bond数下黏性液滴的Rayleigh-Taylor不稳定性

给出了高Bond数下黏性液滴表面Rayleigh-Taylor线性不稳定性的分析解，这种不稳定性对于超音速气流作用下液滴破碎的早期阶段起着至关重要的作用．基于稳定性分析的结果，导出了用于估算稳定液滴的最大直径及液滴无量纲初始破碎时间的计算式，这些计算式与相关文献给出的实验和分析结果比较显示了良好的一致．     

Instability analysis of modulated Taylor vortices

This study investigates the instability analysis of modulated Taylor vortices flow by utilising a numerical method. Based on the consideration that the outer cylinder is fixed and the inner cylinder rotates at a non-zero averaged speed under varying modulated amplitudes and frequencies, the flow is converted from one-dimension Couette flow to Taylor vortices. When the modulated amplitude is greater than 1 and the rotation speed of the inner cylinder exceeds the threshold value for one-dimensional flow, the flow will be more stable at intermediate and high frequencies. When the modulated amplitude is sufficiently large and the inner cylinder rotates at medium frequency, subharmonic flow arises.     

Rayleigh-Taylor instability of an interface in a nonwettable porous medium

The diffusion of vapor through the roof of an underground structure located beneath an aquifer is considered. In the process of evaporation, an interface between the upper water-saturated layer and the lower layer containing an air-vapor mixture is formed. A mathematical model of the evaporation process is proposed and a solution of the steady-state problem is found. It is shown that in the presence of capillary forces in the case of a nonwettable medium the solution is not unique. Using the normal mode method, it is shown that Rayleigh-Taylor instability of the interface can develop in the nonwettable porous medium. It is found that there are two scenarios of loss of stability corresponding to the occurrence of the most unstable wavenumber at zero and at infinity, respectively. It is shown that for zero wavenumber the stability limit is reached at the same time as the solution of the steady-state problem disappears.     

Instability of a slip flow in a curved channel formed by two concentric cylindrical surfaces

Instability of a slip flow in a curved channel formed by two concentric cylindrical surfaces is investigated. Two cases are considered. In the first (Taylor–Couette flow) case the flow is driven by the rotation of the inner cylindrical surface; no azimuthal pressure gradient is applied. In the second case (Dean flow) both cylindrical surfaces are motionless, and the flow is driven by a constant azimuthal pressure gradient. The collocation method is used to find numerically the critical values of the Taylor and Dean numbers, which establish the instability criteria for these two cases. The dependencies of critical values of these numbers on the ratio between the radii of concave and convex walls and on the velocity slip coefficient are investigated.     

Ablative Rayleigh–Taylor instability in the limit of an infinitely large density ratio

The instability of ablation fronts strongly accelerated toward the dense medium under the conditions of inertial confinement fusion (ICF) is addressed in the limit of an infinitely large density ratio. The analysis serves to demonstrate that the flow is irrotational to first order, reducing the nonlinear analysis to solve a two-potential flows problem. Vorticity appears at the following orders in the perturbation analysis. This result simplifies greatly the analysis. The possibility for using boundary integral methods opens new perspectives in the nonlinear theory of the ablative RT instability in ICF. A few examples are given at the end of the Note. To cite this article: P. Clavin, C. Almarcha, C. R. Mecanique 333 (2005).     

Remarks on the Instability of an Incompressible and Isotropic Hyperelastic, Thick-Walled Cylindrical Tube

The problem of instability of a hyperelastic, thick-walled cylindrical tube was first studied by Wilkes [1] in 1955. The solution was formulated within the framework of the theory of small deformations superimposed on large homogeneous deformations for the general class of incompressible, isotropic materials; and results for axially symmetrical buckling were obtained for the neo-Hookean material. The solution involves a certain quadratic equation whose characteristic roots depend on the material response functions. For the neo-Hookean material these roots always are positive. In fact, here we show for the more general Mooney–Rivlin material that these roots always are positive, provided the empirical inequalities hold. In a recent study [2] of this problem for a class of internally constrained compressible materials, it is observed that these characteristic roots may be real-valued, pure imaginary, or complex-valued. The similarity of the analytical structure of the two problems, however, is most striking; and this similarity leads one to question possible complex-valued solutions for the incompressible case. Some remarks on this issue will be presented and some new results will be reported, including additional results for both the neo-Hookean and Mooney–Rivlin materials. This revised version was published online in August 2006 with corrections to the Cover Date.     

Instability of an Interface between Steel Layers Acted upon by an Oblique Shock Wave

This paper reports results of experiments in which development of instability was observed on the interface between two identical metals in tight contact with passage of an oblique shock wave through it. Numerical modeling of experimental results was performed by a twodimensional Lagrangian procedure using an elastoplastic model with a functional dependence of the dynamic yield point on the state variables of the material. The calculations showed that perturbations develop only in the presence of a technological microgap of several tens of micrometers between the metal layers. Unloading of the material behind the oblique shock front into the gap gives rise to a considerable shortterm velocity gradient. Simultaneously, near the interface behind the wave front there is a shortterm loss of strength of the material due to thermal softening and the heterogeneous nature of the deformation.