共查询到20条相似文献,搜索用时 140 毫秒
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以刚性弹体斜侵彻厚靶问题的三维SPH数值模拟研究为工作重点。以三维拉氏有限元流体动力学程序为基础,建立了适用于长杆弹斜侵彻问题研究的刚性弹体与SPH靶体相互耦合的三维数值模拟程序。 相似文献
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研究了Rubin等人提出的基于Rankine卵形体速度势函数分析的侵彻模型。根据该侵彻模型的基本方法编制了计算程序,计算头部形状为锥形、卵形和球形的长杆弹体垂直碰撞靶板时的侵彻深度和穿透靶板后的剩余速度,分析侵彻模型对不同头部形状的长杆弹体的适用性。另外,利用该分析方法计算并分析了卵形头部长杆弹体对铝靶侵彻和穿透的缩比模型问题,用分析方法验证了无量纲侵彻深度和剩余速度相等的侵彻几何相似规律,同时得到了弹体减加速度与几何尺寸成反比的重要结论。最后对混凝土靶板的侵彻与穿透问题进行了尝试计算,得到了同实验基本一致的计算结果并对其进行了深入分析。 相似文献
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采用光滑粒子流体动力学(SPH)方法对花岗岩靶板受碰撞侵彻的大应变、高应变率变形问题进行了数值模拟。为了描述弹目材料的非线性变形及破坏特性,对花岗岩靶板引入了Holmquist-Johnson-Cook(HJC)本构模型及损伤模型,对弹体引入含损伤的Johnson-Cook(J-C)本构方程和Grüneisen状态方程,靶板与弹体均离散成拉格朗日粒子。通过自编程序仿真计算0~4 m/s的着靶速度下花岗岩靶板的三维侵彻过程,对比分析了钢珠在不同弹体条件下的侵彻结果,在固体侵彻、半流体侵彻和流体侵彻的区域内拟合了侵彻深度随着靶速度的变化曲线。数值计算结果显示,侵彻深度随着靶速度的增加在固体侵彻区间(v01421 m/s)呈现递增趋势,在半流体侵彻区间(1421 m/s?v0?1700 m/s)呈现递减趋势,在流体侵彻区间(v0 1700 m/s)呈现递增趋势并逐渐趋于平滑,达到峰值。 相似文献
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在对混凝土动态力学性能和现有本构模型综合分析的基础上,构建了一个新的适用于冲击响应问题数值分析的混凝土本构模型。该本构模型全面考虑了压力、应力第三不变量、变形的硬化和软化、应变率强化以及拉伸损伤等各个影响因素。将其加入LTZ-2D程序,确定了本构模型参数,对混凝土靶板的穿透问题进行了数值验证分析。计算得到的弹体剩余速度同实验结果基本一致,同时得到了混凝土靶板破裂的计算图像。计算结果及其分析表明,所构建的本构模型能够较好地反映冲击载荷作用下混凝土动态响应的主要特性。 相似文献
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《高压物理学报》2021,35(5)
为研究不同算法对弹体侵彻花岗岩模拟的影响,基于仿真分析软件LS-DYNA中的Lagrange算法及SPH(Smooth particle hydrodynamics)算法,采用Lagrange、SPH-Lagrange耦合及SPH算法分别对弹体侵彻、贯穿花岗岩靶体进行数值模拟,并从计算效率、侵彻深度、速度衰减、靶体损伤、Mises应力分布多方面对比模拟结果,分析3种算法用于研究岩石侵彻问题的优势和不足。研究表明:Lagrange算法的计算效率最高,计算精度高,但存在单元畸变、无撞击溅射、无后坑区等问题;SPH算法的计算效率最低,但模拟效果良好;SPH-Lagrange耦合算法兼具二者优势,但会导致应力滞后和应力波不稳定衰减。在大型模拟中应优先选用Lagrange算法和SPH-Lagrange耦合算法。 相似文献
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利用LS-DYNA3D软件数值计算了弹体侵彻岩石、混凝土和土问题,分析在不同碰撞速度条件下的弹体响应和靶体抗侵彻能力。碰撞速度小于900 m/s时,弹体侵彻岩石的减加速度峰值约是侵彻混凝土的2倍,而侵彻混凝土的减加速度峰值约是侵彻土的6倍。减加速度峰值高则稳态侵彻过程短,弹体能量消耗很快。碰撞速度超过1.5 km/s时,随靶体材料的强度、密度逐渐减小,侵彻深度和孔径逐渐缓慢增加,岩石、混凝土和土3种靶体材料相比,最大侵彻深度增加41%~62%,最大扩孔口径增加16%~25%。 相似文献
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提出了一种最小二乘粒子有限元方法,用其模拟了二维水珠滴落水面并飞溅散开的过程.该法基于拉格朗日描述,在每个时间步上使用扩展的Delaunay划分更新计算网格,并应用α形方法识别自由面形状;用最小二乘有限元方法离散流体运动的Navier-Stokes方程,并推导了一种自适应时间步长方案以提高计算效率和鲁棒性;引入网格拉伸技术修正减小流体质量误差.对水滴飞溅进行仿真,得到了与商用软件Flow-3d比较符合的结果,且具有更清晰锐利的自由面.
关键词:
滴落
网格划分
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最小二乘有限元 相似文献
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In this paper, a new simple meshless method is presented for the solution of incompressible inviscid fluid flow problems with moving boundaries. A Lagrangian formulation established on pressure, as a potential equation, is employed. In this method, the approximate solution is expressed by a linear combination of exponential basis functions (EBFs), with complex-valued exponents, satisfying the governing equation. Constant coefficients of the solution series are evaluated through point collocation on the domain boundaries via a complex discrete transformation technique. The numerical solution is performed in a time marching approach using an implicit algorithm. In each time step, the governing equation is solved at the beginning and the end of the step, with the aid of an intermediate geometry. The use of EBFs helps to find boundary velocities with high accuracy leading to a precise geometry updating. The developed Lagrangian meshless algorithm is applied to variety of linear and nonlinear benchmark problems. Non-linear sloshing fluids in rigid rectangular two-dimensional basins are particularly addressed. 相似文献
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Modeling Three-Dimensional Multiphase Flow Using a Level Contour Reconstruction Method for Front Tracking without Connectivity 总被引:3,自引:0,他引:3
Three-dimensional multiphase flow and flow with phase change are simulated using a simplified method of tracking and reconstructing the phase interface. The new level contour reconstruction technique presented here enables front tracking methods to naturally, automatically, and robustly model the merging and breakup of interfaces in three-dimensional flows. The method is designed so that the phase surface is treated as a collection of physically linked but not logically connected surface elements. Eliminating the need to bookkeep logical connections between neighboring surface elements greatly simplifies the Lagrangian tracking of interfaces, particularly for 3D flows exhibiting topology change. The motivation for this new method is the modeling of complex three-dimensional boiling flows where repeated merging and breakup are inherent features of the interface dynamics. Results of 3D film boiling simulations with multiple interacting bubbles are presented. The capabilities of the new interface reconstruction method are also tested in a variety of two-phase flows without phase change. Three-dimensional simulations of bubble merging and droplet collision, coalescence, and breakup demonstrate the new method's ability to easily handle topology change by film rupture or filamentary breakup. Validation tests are conducted for drop oscillation and bubble rise. The susceptibility of the numerical method to parasitic currents is also thoroughly assessed. 相似文献
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CHAP3D是北京应用物理与计算数学研究所自主研发的Lagrange通用弹塑性流体力学分析程序.文章介绍了在CHAP3D程序中使用的、针对多处理器集群的、基于静态双重区域分解的两种接触并行算法.第一种是分配单个完整接触面的接触并行算法,此算法将一对完整的接触面分配到一个处理器上,并建立计算域与接触域的通信关系.此接触并行算法的优点是简单,在具有接触面的处理器上可以直接使用串行的接触搜索算法和接触力耦合计算算法.另一种是主面剖分区域分解的接触并行算法,此算法将所有接触面的主面区域分解到所有处理器上.须建立计算域与接触域以及接触域内各处理器间的两种通信关系.该接触并行算法是一个负载平衡的并行算法,具有很好的并行效率和可扩展性.数值算例显示,这两种接触并行算法都能够很好地模拟多种不同类型的接触问题. 相似文献
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A new method of absolute phase evaluation for three-dimensional (3D) profile measurement using fringe projection is presented, which combines the gray code and the phase shift technique. Two kinds of fringe patterns are projected onto the object surface respectively, one is sinusoidal intensity distribution used for phase demodulation and the other is gray code fringe pattern for unwrapping. These images are acquired by camera and stored into computer. The absolute phase is obtained by analyzing these images. The validity of this method is verified experimentally. The method is superior to other phase unwrapping methods. 相似文献
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We present a computational method for determining the geometry of a class of three-dimensional invariant manifolds in non-autonomous (aperiodically time-dependent) dynamical systems. The presented approach can be also applied to analyse the geometry of 3D invariant manifolds in three-dimensional, time-dependent fluid flows. The invariance property of such manifolds requires that, at any fixed time, they are given by surfaces in R3. We focus on a class of manifolds whose instantaneous geometry is given by orientable surfaces embedded in R3. The presented technique can be employed, in particular, to compute codimension one (invariant) stable and unstable manifolds of hyperbolic trajectories in 3D non-autonomous dynamical systems which are crucial in the Lagrangian transport analysis. The same approach can also be used to determine evolution of an orientable ‘material surface’ in a fluid flow. These developments represent the first step towards a non-trivial 3D extension of the so-called lobe dynamics — a geometric, invariant-manifold-based framework which has been very successful in the analysis of Lagrangian transport in unsteady, two-dimensional fluid flows. In the developed algorithm, the instantaneous geometry of an invariant manifold is represented by an adaptively evolving triangular mesh with piecewise C2 interpolating functions. The method employs an automatic mesh refinement which is coupled with adaptive vertex redistribution. A variant of the advancing front technique is used for remeshing, whenever necessary. Such an approach allows for computationally efficient determination of highly convoluted, evolving geometry of codimension one invariant manifolds in unsteady three-dimensional flows. We show that the developed method is capable of providing detailed information on the evolving Lagrangian flow structure in three dimensions over long periods of time, which is crucial for a meaningful 3D transport analysis. 相似文献