无氧铜层裂的实验与数值研究

利用一级气体炮对国产的无氧铜（OFHC）进行了平板撞击致层裂实验,3 mm厚的OFHC飞片撞击6 mm厚的OFHC靶,采用锰铜应力计记录试样/有机玻璃（PMMA）界面附近的应力历史,获得试样发生层裂的信息。软回收试样,观测回收试样的层裂片。采用基于空穴聚集的层裂模型,数值模拟这些平板撞击致层裂实验。数值模拟的应力剖面以及试样层裂片厚度与实验结果基本一致。此外,对于国外相关的OFHC层裂实验,采用基于空穴聚集的层裂模型也作了相应的数值模拟,并进行了比较。     

钢圆管在内爆加载下的层裂特性研究

利用完整回收技术,获得了20钢圆管在不同固体装药厚度、装药类型以及外壳条件的滑移内爆加载下形变和层裂的特征和规律,得到了钢圆管层裂的相对临界装药厚度等初步结果,分析了装药类型、装药厚度、外壳对钢圆管层裂的影响。     

液体炸药滑移内爆加载下钢管的变形与层裂破坏研究

用液体炸药滑移内爆加载方式,研究了不同炸药厚度和外壳条件下20钢圆管的内聚变形和破坏特征。实验中,钢管发生了较大径向应变,应变值大致随炸药厚度的增加而线性增大。在炸药厚度不低于3mm时钢管变形均匀,轴对称较好;药厚小于3mm时其变形不再是基本轴对称收缩,管子表面出现扭转褶皱。各种装药厚度下,均未观察到预期的层裂破坏。对未层裂的原因进行了初步分析。     

马赫杆加载下无氧铜的动态破碎

为了深入了解金属材料在复杂加载下的动态破碎行为,在有限元模拟的基础上,设计了两类马赫杆加载实验,用于研究无氧铜在复杂加载下的动态破碎行为。实验中,采用火炮加载马赫透镜和激光粒子速度干涉仪测量自由面速度,实现了峰值压力分别为95.75和32.38 GPa的动态加载。结果表明,实验中成功实现了稳定的马赫杆加载,并且观察到马赫杆加载下无氧铜的2种不同近表面破碎模式,即高压下产生微层裂、低压下产生三角波层裂,且层裂区呈凸形分布。

     

滑移爆轰驱动钢管的层裂

将VG损伤模型推广到二维情况,考虑了最大主应力方向对损伤演化的影响,并使用显式断裂算法对20钢管在GI-920炸药滑移爆轰驱动下层裂的问题进行二维数值模拟。分析了一维内爆和滑移爆轰两种加载方式下作用于钢管外表面的压力及钢管内部受力状态的区别,考察了滑移爆轰加载方式下钢管外表面的受力随炸药厚度变化的规律,进而研究了钢管内损伤的分布和演化,以及裂纹的产生和扩展现象。计算得到的层裂片初始厚度随炸药厚度的变化规律与实验结果符合较好。     

混凝土材料的层裂特性

利用Hopkinson压杆作为实验设备,通过试件后面吸收杆上应变波形研究了混凝土材料的层裂特性。不同强度混凝土在不同加载率下的实验结果表明,混凝土层裂强度与其压缩强度以及加载速率有关,给出了层裂强度和压缩强度以及加载率之间关系的经验公式,并指出不同加载速度下混凝土裂纹扩展方式不同是层裂强度率效应的主要原因。加载压缩波损伤的影响、重复加载实验以及多次层裂的顺序都表明,损伤对混凝土的层裂过程有重要影响。     

高导无氧铜的临界冲击拉伸速度

基于气炮系统,提出了一种新的临界冲击拉伸速度实验方法。实验装置主要由2部分组成:气体炮系统驱动弹丸和弹丸击靶牵引多根拉伸杆试件。采用该实验方法对高导无氧铜进行了临界冲击拉伸速度实验。对于一维应力的临界冲击拉伸速度实验,探讨了一种完全热耦合的在颈缩区域计及塑性约束系数以及空穴增长与聚集效应的数值模拟方法。高导无氧铜的临界冲击拉伸速度实验的数值模拟结果表明,采用Zerilli-Armstrong本构关系预估的实验临界冲击拉伸速度比采用Johnson-Cook本构关系预估的更符合实验。     

金属材料层裂破坏的内聚力模型

为了考虑层裂破坏过程中能量耗散行为,论文把内聚力单元嵌入到连续介质有限元单元之间,从而构建了一个层裂破坏的内聚力模型.随后采用该模型对平板撞击条件下的20号钢层裂实验进行了数值模拟研究,重点讨论了内聚力模型特征参数对计算结果的影响规律.研究结果表明采用指数型损伤演化行为的内聚力模型可以较好地描述层裂破坏过程中的能量耗散行为.利用一发实测自由面速度波剖面对计算结果进行校准,确定内聚力模型特征参数.该特征参数可以用于模拟不同撞击速度下的层裂实验,获得的模拟曲线与实验曲线之间符合程度很好,特别是自由面速度“回跳”后波形振荡周期和幅值与实验结果非常接近,这表明了内聚力模型在描述层裂过程中能量耗散行为方面具有较好适用性,并且其参数也具有很好的可移植性.     

混凝土层裂强度测量的新方法

提出了利用Hopkionson压杆测量混凝土层裂强度的新实验方法:用高聚物材料取代传统的金属材料透射杆,混凝土试件为细长杆,由于高聚物波阻抗比混凝土小,试件中压缩波在试件/吸收杆界面反射后形成拉伸波使试件产生层裂破坏,通过吸收杆上透射波形可以确定混凝土层裂强度。由于波在粘弹性材料中的弥散效应,吸收杆中透射波形会发生变化,但三维有限元分析表明,在利用吸收杆上透射波确定混凝土层裂强度时弥散产生的影响可以忽略。按照一维特征线理论,可以由吸收杆上的应变波形确定出混凝土材料的层裂强度。     

FeMnNi合金的冲击相变和层裂特性的实验研究

对FeMnNi合金进行了轻气炮平板撞击实验研究,实验中材料发生了相变和层裂。得到的FeMnNi合金的相变阈值压力为6.3~6.9 GPa,远低于纯铁的相变阈值压力13 GPa,说明Mn、Ni合金元素的加入会极大的降低相变阈值。回收试样观测表明,当应力高于FeMnNi合金的相变阈值时,样品中可能产生二次层裂现象和浅表层裂新现象。实验结果还表明该合金相变后层裂强度没有明显的提高。     

Dynamic characteristics of spherically converging detonation waves

The spherically converging detonation wave was numerically investigated by solving the one-dimensional multi-component Euler equations in spherical coordinates with a dispersion-controlled dissipative scheme. Finite rate and detailed chemical reaction models were used and numerical solutions were obtained for both a spherical by converging detonation in a stoichiometric hydrogen-oxygen mixture and a spherically focusing shock in air. The results showed that the post-shock pressure approximately arises to the same amplitude in vicinity of the focal point for the two cases, but the post-shock temperature level mainly depends on chemical reactions and molecular dissociations of a gas mixture. While the chemical reaction heat plays an important role in the early stage of detonation wave propagation, gas dissociations dramatically affect the post-shock flow states near the focal point. The maximum pressure and temperature, non-dimensionalized by their initial value, are approximately scaled to the propagation radius over the initial detonation diameter. The post-shock pressure is proportional to the initial pressure of the detonable mixture, and the post-shock temperature is also increased with the initial pressure, but in a much lower rate than that of the post-shock pressure. Zonglin Jiang is presently a visiting professor at McGill University, Canada.     

内聚滑移爆轰加载下金属圆管压缩过程的工程分析

对内聚滑移爆轰加载下圆管压缩运动过程进行工程分析,分析解与数值模拟结果吻合。利用工程模型得到了不同管道参数（包括内径、厚度）下管道封闭所需要的炸药量和封闭时间表达式,可为相关研究工作提供参考。

     

Stability of converging cylindrical shock waves

An experimental and numerical study was made of converging cylindrical shock waves. The goal of the present study was to clarify the movement and instability of the converging cylindrical shock waves. Experiments were conducted in an annular shock tube of 230 mm o.d. and 210 mm i.d. connected to a cylindrical test section of 210 mm diameter. Double exposure holographic interferometry was used to visualize the converging cylindrical shock waves. Incident shock Mach numbers ranged between 1.1 and 2.0 in air. A numerical simulation was conducted using the TVD finite difference scheme. It was found in the experiments that although the initial shock wave configuration looked cylindrical, it was gradually deformed with propagation towards the center and finally showed mode-four instability. This is attributable to the existence of initial disturbances which were introduced by the struts which supported the inner tube of the annular shock tube. This trend was significant for stronger shock waves indicating that at the last stage of shock wave convergence the initial perturbations of the converging cylindrical shock wave were amplified to form the triple point of Mach reflection. The numerical results correctly predicted the experimental trend.This article was processed using Springer-Verlag T_EX Shock Waves macro package 1990.     

圆柱形爆轰波的二维数值模拟

基于带化学反应的二维Euler方程,对圆柱形爆轰波的直接起爆和传播过程进行了二维数值模拟研究,拟分析起爆条件和初始压强对圆柱形爆轰波形成和传播的影响。研究发现,圆柱形爆轰波起爆成功向外传播的过程中,新的三波结构的生成标志着爆轰波进入稳定传播阶段。在起爆能量足够的情况下,起爆半径(曲率)的大小决定着三波结构初始形成时的数目和传播半径,起爆压强对其基本不产生影响;起爆半径大(曲率小)时,三波结构初始形成时的传播半径大、数目多,圆柱形爆轰波进入稳定传播阶段的传播距离长;数值模拟中,初始压强的提高,有助于圆柱形爆轰在较短的传播距离内进入稳定传播阶段。     

爆轰法合成碳包覆纳米铜颗粒

以硝酸铜和柠檬酸制成的干凝胶为主要反应物,加入油酸有机碳源和黑索今炸药,在氮气保护气氛下在爆炸容器中引爆,成功地合成了碳包覆纳米铜颗粒。分别采用X射线衍射、透射电镜对产物形貌特征进行表征。结果表明,在爆轰产物中富含碳包覆纳米铜颗粒,产物呈圆球体,具有完好的核壳结构形貌,颗粒粒径在10~40nm 之间,外层碳壳结构主要由无定型碳和石墨构成。并对爆轰法合成碳包覆纳米铜颗粒的形成机理进行了分析。     

球状纳米铜颗粒的爆轰法制备

以乙酸铜为前躯体,并与液体石蜡和黑索今(RDX)炸药充分混合,在真空爆轰反应容器中引爆,制备球状纳米铜晶。采用透射电镜(TEM)、X射线衍射(XRD)研究了爆轰产物的形貌和成分,同时通过Raman光谱仪对爆轰产物中碳的结构进行了分析。结果显示,纳米铜晶具有较完整的球状结构,颗粒表面光滑,直径集中分布在150~200nm 之间。爆轰法可为制备圆整度好的纳米铜提供一种简单、快捷的方法。     

Experimental study on a heavy-gas cylinder accelerated by cylindrical converging shock waves

The Richtmyer–Meshkov instability behavior of a heavy-gas $(\text{ SF }_6)$ cylinder accelerated by a cylindrical converging shock wave is studied experimentally. A curved wall profile is well-designed based on the shock dynamics theory [Phys. Fluids, 22: 041701 (2010)] with an incident planar shock Mach number of 1.2 and a converging angle of $15^\circ $ in a $95\,\text{ mm }\times 95$ mm square cross-section shock tube. The $\text{ SF }_6$ cylinder mixed with the glycol droplets flows vertically through the test section and is illuminated horizontally by a laser sheet. The images obtained only one per run by an ICCD (intensified charge coupled device) combined with a pulsed Nd:YAG laser are first presented and the complete evolution process of the $\text{ SF }_6$ cylinder is then captured in a single test shot by a high-speed video camera combined with a high-power continuous laser. In this way, both the developments of the first counter-rotating vortex pair and the second counter-rotating vortex pair with an opposite rotating direction from the first one are observed. The experimental results indicate that the phenomena induced by the converging shock wave and the reflected shock formed from the center of convergence are distinct from those found in the planar shock case.     

叠氮化铜微装药爆轰驱动飞片的数值模拟

为了优化叠氮化铜微装药器件的设计,探究叠氮化铜爆轰驱动飞片的作用原理,根据微装药器件的实际设计和相关实验,采用ANSYS/LS-DYNA流固耦合算法对叠氮化铜爆轰驱动飞片的作用过程作了数值模拟。具体研究了加速膛长度对飞片的平整性和完整性的影响,分析了微装药的尺寸与飞片速度之间的关系。研究结果表明:加速膛的长度对飞片的完整性、平整性和速度具有重要影响,在过长的加速膛中飞片飞行时易发生破碎,加速膛过短飞片的驱动速度不能达到最佳。装药尺寸与飞片速度之间关系密切,装药直径对飞片速度的前期成长影响不大,但对飞片获得的最大速度却有较为明显的影响;装药的直径大于0.8 mm时,增加装药直径并不能使飞片的最大速度明显增加。     

Numerical investigation on evolution of cylindrical cellular detonation

Cylindrical cellular detonation is numerically investigated by solving two- dimensional reactive Euler equations with a finite volume method on a two-dimensional self-adaptive unstructured mesh. The one-step reversible chemical reaction model is applied to simplify the control parameters of chemical reaction. Numerical results demonstrate the evolution of cellular cell splitting of cylindrical cellular detonation explored in experimentas. Split of cellular structures shows different features in the near-field and far-field from the initiation zone. Variation of the local curvature is a key factor in the behavior of cell split of cylindrical cellular detonation in propagation. Numerical results show that split of cellular structures comes from the self-organization of transverse waves corresponding to the development of small disturbances along the detonation front related to detonation instability.