基于SPH方法的表面张力修正算法及其应用

针对传统SPEI方法中基于CSF模型的表面张力算法,在计算边界、尖角等粒子缺失部位的曲率时存在偏差较大,且粒子秩序较差,对大变形问题表面张力计算精度较低的问题,在Morris提出的表面张力SPH方法基础上,通过引入CSPM方法对边界法向的计算和曲率的计算进行修正,得到了表面张力修正方程组.应用本文方法模拟了水溶液中初始...     

一种可考虑界面不连续的改进SPH方法

SPH方法模拟工程问题时通常遇到不连续的物理量,因此有必要引入不连续的SPH方法.本文基于Taylor展开公式推导了2D和3D的不连续SPH公式.针对越过材料界面不连续物理量的计算,给出了大变形计算中确定不连续位置的方法,基于Taylor展开公式,从理论上给出了确定不连续公式中x_(k)点的方法,并用数值方法验证了此方法的有效性.比较和讨论了初始SPH方法,CSPM方法与不连续SPH方法处理不连续量的效果.结果显示不连续SPH方法在计算不连续量时有较大的优势.     

多化学组份反应气体流动的Godunov格式

本文将单介质气体流动的Goduoov方法推广到多化学组份气体流动的计算中,建立了多化学组份气体的间断分解公式以及任意四边形网格下的Godunov方法的差分格式,提出了处理自由边界的虚相法,应用第二类网格,计算了超音速射流及其冲击问题的几个算例,并且同实验结果进行了比较。     

基于SPH的动力松弛法

光滑质点流体动力学方法(SPH;Smoothed Particle Hydrodynamics)是一种新的纯Lagrangian方法,由于该方法在计算空间导数的时候不需要借助于网格,从而避免了Lagrangian网格在处理大变形问题时的缠结和扭曲问题.传统上,SPH方法主要用来模拟天体问题以及流体或固体的动力问题.动力松弛法(DR;Dynamic Relax-ation)通过采用虚拟质量和虚拟阻尼将一个静力问题转化为动力问题,最早用于解决潮汐问题.DR方法从数学的角度来说是一种求解线性方程组的方法,并不涉及连续结构的离散.所以采用网格方法离散时,DR方法同样受到网格变形导致计算精度下降的困扰.论文采用SPH离散连续体,然后用DR方法求解结构的平衡状态,并根据SPH的特点,提出一种加速收敛的新型计算方法.     

双曲偏微分方程的局部伪弧长方法研究

重点研究了局部伪弧长方法在处理偏微分方程,尤其是双曲型偏微分方程出现激波间断的奇异性问题,对比分析了全局伪弧长方法空间转化的形式及其网格自适应的性质。为提高求解效率,提出了局部伪弧长方法,利用激波间断的性质,给出了判断奇异点位置以及模板选择的方法,涉及如何处理激波振荡,如何引入弧长参数,以及怎样求解间断等问题。通过数值算例验证了局部伪弧长在激波捕捉和追踪方面的可行性,通过比较局部伪弧长方法与Godunov方法处理不同初值条件的双曲问题,显示出局部伪弧长方法处理双曲偏微分方程的优越性,为伪弧长方法应用到物理问题奠定基础。     

二维空间中基于黎曼解的SPH方法

应用传统的光滑粒子流体动力学(SPH)方法模拟激波问题能自主捕获波阵面,但是在接触间断界面处却不可避免地存在压力振荡。采用黎曼解修正粒子对之间的相互作用,并将基于黎曼解的SPH方法扩展到二维空间。通过对一维具有解析解的激波管问题和二维拟内爆问题的模拟,比较了基于黎曼解的SPH方法和传统的SPH方法。数值结果表明,相对于传统的SPH方法,基于黎曼解的SPH方法能够有效避免接触界面处的压力振荡,提高求解的精度。     

一种简单的精确捕捉接触间断的黎曼求解器

基于Godunov型数值格式的有限体积法是求解双曲型守恒律系统的主流方法,其中用来计算界面数值通量的黎曼求解器在很大程度上决定了数值格式在计算中的表现。单波的Rusanov求解器和双波的HLL求解器具有简单、高效和鲁棒性好等优点,但是在捕捉接触间断时耗散太大。全波的HLLC格式能够精确捕捉接触间断,但是在计算中出现的激波不稳定现象限制了其在高马赫数流动问题中的应用。本文利用双曲正切函数和五阶WENO格式来重构界面两侧的密度值,并且结合边界变差下降算法来减小Rusanov格式耗散项中的密度差,从而提高格式对于接触间断的分辨率。研究表明,相比于全波的HLLC求解器,本文构造的黎曼求解器不仅具有更高的接触分辨率,而且还具有更好的激波稳定性。     

计算反平面裂纹应力强度因子K_Ⅲ的位移间断法

本文采用Fourier变换,推导了纵向剪切问题间断位移、周期间断位移以及半平面间断位移的理论解,并由此建立了一组求解含裂纹与孔洞问题的线性方程。几个较为复杂的数值算例证明了本方法具有较高的精度和好的收敛性。     

求解可压缩流的二维通量分裂格式

传统的一维通量分裂格式在计算界面数值通量时,只考虑网格界面法向的波系。采用传统的TV格式分别求解对流通量和压力通量。通过求解考虑了横向波系影响的角点数值通量来构造一种真正二维的TV通量分裂格式。在计算一维数值算例时,该格式与传统的TV格式具有相同的数值通量计算公式,因此其保留了传统的TV格式精确捕捉接触间断和膨胀激波的优点。在计算二维算例时,该格式比传统的TV格式具有更高的分辨率;在计算二维强激波问题时,消除了传统TV格式的非物理现象,表现出更好的鲁棒性;此外,该格式大大提高了稳定性CFL数,从而具有更高的计算效率。因此,本文方法是一种精确、高效并且具有强鲁棒性的数值方法,在可压缩流的数值模拟中具有广阔的应用前景。     

一种处理弹性动力边界元法中奇异积分的方法

利用边界元法求解瞬态弹性动力学问题时,时域基本解函数的分段连续性和奇异性为该问题的求解带来很大的困难。为了解决时域基本解中的奇异性问题,本文依据柯西主值的定义,对经过时间解析积分之后的时域基本解进行奇异值分解,将其分成奇异和正则积分两部分;其中正则部分可通过采用常规高斯积分方法来计算,而奇异部分具有简单的形式,可以利用解析积分计算。经过上述操作之后,就可以达到直接消除时域基本解中奇异积分的目的。和传统方法相比,本文方法并不依赖静力学基本解来消除奇异性,是一种直接求解方法。最后给定两个数值算例来验证本文提出方法的正确性和可行性,结果表明使用本文算法可以解决弹性动力学边界积分方程中的奇异性问题。     

Efficient meshless SPH method for the numerical modeling of thick shell structures undergoing large deformations

The objective of this paper is to present an extension of the Lagrangian Smoothed Particle Hydrodynamics (SPH) method to solve three-dimensional shell-like structures undergoing large deformations. The present method is an enhancement of the classical stabilized SPH commonly used for 3D continua, by introducing a Reissner–Mindlin shell formulation, allowing the modeling of moderately thin structure using only one layer of particles in the shell mid-surface. The proposed Shell-based SPH method is efficient and very fast compared to the classical continuum SPH method. The Total Lagrangian Formulation valid for large deformations is adopted using a strong formulation of the differential equilibrium equations based on the principle of collocation. The resulting non-linear dynamic problem is solved incrementally using the explicit time integration scheme, suited to highly dynamic applications. To validate the reliability and accuracy of the proposed Shell-based SPH method in solving shell-like structure problems, several numerical applications including geometrically non-linear behavior are performed and the results are compared with analytical solutions when available and also with numerical reference solutions available in the literature or obtained using the Finite Element method by means of ABAQUS^© commercial software.     

改进的SPH边界处理方法与土体大变形模拟

沙土滑坡往往会造成重大的人身财产损失,研究这类土体大变形问题对防灾工程具有指导意义。光滑粒子流体动力学SPH（Smoothed Particle Hydrodynamics）方法是一种拉格朗日型无网格粒子法,十分适用于模拟大变形问题。在SPH方法中,合适的边界处理方法一直是个难点,传统的边界虚粒子法或排斥力法较难模拟复杂边界。本文引入了一种能处理任意形状边界的方法——统一半解析壁面边界条件处理方法USAW（unified semi-analytical wall boundary conditions）,通过在控制方程中引入修正因子并保留边界面积分项来弥补边界缺失。为了更准确模拟问题域边界,提出无质量边界粒子的新概念。利用该方法成功模拟了土体滑坡算例,验证了方法的可靠性,并避免了边界零粒子层问题。通过数值模拟,分析了内摩擦角和黏聚力等土体物性参数对滑坡过程的影响。最后,应用该方法研究了滑坡冲击楔形体时的压力响应。     

Simulations of single bubbles rising through viscous liquids using Smoothed Particle Hydrodynamics

The shapes and dynamics of single bubbles rising through viscous fluids are studied using the SPH (Smoothed Particle Hydrodynamics) approach. This fully Lagrangian, particle-based method is applied to compute the complete two-phase flow, both inside the bubbles as well as around them. For that purpose, a multi-phase formulation of the SPH method that can address large density differences is retained, while surface tension effects are explicitly accounted for through a CSF (Continuum Surface Force) model. Numerical simulations have been performed for different regimes (corresponding to different relative importance of surface tension, viscosity and buoyancy effects) and the predicted topological changes as well as the terminal velocity and drag coefficients of bubbles are validated. The numerical outcomes are assessed not only with respect to reference experimental data but also with respect to other numerical methods, namely the Front-Tracking and the Lattice Boltzmann Methods. It is believed that this study corresponds to a new application of SPH approaches for two-phase flow simulations and results reveal the interest of this method to capture fine details of gas–liquid systems with deformable and rapidly changing interfaces.     

SPH modeling of fluid–solid interaction for dynamic failure analysis of fluid-filled thin shells

This work concerns the prediction of failure of a fluid-filled tank under impact loading, including the resulting fluid leakage. A water-filled steel cylinder associated with a piston is impacted by a mass falling at a prescribed velocity. The cylinder is closed at its base by an aluminum plate whose characteristics are allowed to vary. The impact on the piston creates a pressure wave in the fluid which is responsible for the deformation of the plate and, possibly, the propagation of cracks. The structural part of the problem is modeled using Mindlin–Reissner finite elements (FE) and Smoothed Particle Hydrodynamics (SPH) shells. The modeling of the fluid is also based on an SPH formulation. The problem involves significant fluid–structure interactions (FSI) which are handled through a master–slave-based method and the pinballs method. Numerical results are compared to experimental data.     

基于拟流体模型的SPH新方法及其在弹丸超高速碰撞薄板中的应用

引入颗粒动力学理论(拟流体模型)建立了适用于超高速碰撞的SPH新方法。将超高速碰撞中处于损伤状态的碎片等效为拟流体,在描述其运动过程中引入了碎片间相互作用和气体相对碎片的作用。采用该方法对球形弹丸超高速碰撞薄板形成碎片云的过程进行了数值模拟,得到了弹坑直径、外泡碎片云和内核碎片云的形状、分布,并与使用传统SPH方法、自适应光滑粒子流体动力学(ASPH)方法的模拟结果进行对比,结果显示:新方法在内核碎片云形状和分布上计算结果更加准确。同时对Whipple屏超高速碰撞问题进行了研究,分析了不同撞击速度下防护屏弹坑尺寸及舱壁损伤特性等特性,计算结果与实验吻合较好且符合Whipple防护结构的典型撞击极限曲线。     

Prediction of energy losses in water impacts using incompressible and weakly compressible models

In the present work the simulation of water impacts is discussed. The investigation is mainly focused on the energy dissipation involved in liquid impacts in both the frameworks of the weakly compressible and incompressible models. A detailed analysis is performed using a weakly compressible Smoothed Particle Hydrodynamics (SPH) solver and the results are compared with the solutions computed by an incompressible mesh-based Level-Set Finite Volume Method (LS-FVM). Impacts are numerically studied using single-phase models through prototypical problems in 1D and 2D frameworks. These problems were selected for the conclusions to be of interest for, e.g., the numerical computation of the flow around plunging breaking waves. The conclusions drawn are useful not only to SPH or LS-FVM users but also for other numerical models, for which accurate results on benchmark test-cases are provided.     

A one-dimensional meshfree particle formulation for simulating shock waves

In this paper, a one-dimensional meshfree particle formulation is proposed for simulating shock waves, which are associated with discontinuous phenomena. This new formulation is based on Taylor series expansion in the piecewise continuous regions on both sides of a discontinuity. The new formulation inherits the meshfree Lagrangian and particle nature of SPH, and is a natural extension and improvement on the traditional SPH method and the recently proposed corrective smoothed particle method (CSPM). The formulation is consistent even in the discontinuous regions. The resultant kernel and particle approximations consist of a primary part similar to that in CSPM, and a corrective part derived from the discontinuity. A numerical study is carried out to examine the performance of the formulation. The results show that the new formulation not only remedies the boundary deficiency problem but also simulates the discontinuity well. The formulation is applied to simulate the shock tube problem and a 1-D TNT slab detonation. It is found that the proposed formulation captures the shock wave at comparatively lower particle resolution. These preliminary numerical tests suggest that the new meshfree particle formulation is attractive in simulating hydrodynamic problems with discontinuities such as shocks waves.Received: 8 October 2002, Accepted: 10 May 2003, Published online: 15 August 2003     

三维自适应FE-SPH耦合算法在多层间隔金属靶侵彻问题中的应用

鉴于有限元算法不能有效地模拟侵彻过程所产生的金属碎片, 本文中基于三维自适应FE-SPH耦合算法的基本理论, 自主开发了模拟多层间隔金属靶侵彻问题的三维FE-SPH耦合计算程序。该程序采用四面体单元对多层间隔金属靶侵彻模型进行初始离散, 计算过程中, 当四面体单元等效塑性应变超过某一设定值时, 单元自动转化为SPH粒子, 并引入有限单元-粒子接触算法和耦合算法, 实现大变形和破碎区域采用SPH方法计算, 克服有限元法单元畸变存在的问题。多层间隔靶侵彻算例分析表明, 三维FE-SPH耦合计算程序采用等效塑性应变作为转化判据计算结果较稳定, 并且能够有效地再现侵彻过程中所产生的碎片, 能够模拟侵彻碎片对后层靶的毁伤效应。     

A detailed study of lid‐driven cavity flow at moderate Reynolds numbers using Incompressible SPH

Lid‐driven cavity flow at moderate Reynolds numbers is studied here, employing a mesh‐free method known as Smoothed Particle Hydrodynamics (SPH). In a detailed study of this benchmark, the incompressible SPH approach is applied together with a particle shifting algorithm. Additionally, a new treatment for no‐slip boundary conditions is developed and tested. The use of the aforementioned numerical treatment for solid walls leads to significant improvements in the results with respect to other SPH simulations carried out with similar spatial resolution. However, the effect of spatial resolution is not considered in the present study as the number of particles used in each case was kept constant, approximately reproducing the same resolutions employed in reference studies available in the literature as well. Altogether, the detailed comparisons of field variables at discreet points demonstrate the accuracy and robustness of the new SPH method. Copyright © 2014 John Wiley & Sons, Ltd.