非均匀炸药冲击起爆和起爆后的行为

 介绍并分析了Campbell 等人及其他作者研究非均匀炸药冲击起爆和起爆后行为所获得的实验结果,但不涉及其冲击起爆条件。足够强的冲击波进入非均匀炸药后,爆轰将瞬时（指不经过感应时间）且直接（指不经过其他过程,如爆燃）被引发;非均匀炸药起爆后,其中传播的自始至终是一个不断增长的爆轰波,直至发展为正常爆轰,整个过程都是爆轰的增长（新定义）过程。不存在由反应冲击波不断增长并转变为爆轰波的所谓向爆轰的增长。所谓向爆轰的增长,实际上是爆轰的增长（按新定义）的初期;Craig原定义的爆轰的增长,实际上是爆轰的增长（按新定义）的后期;而所谓反应冲击波,实际上是增长中的初期爆轰波。爆轰的增长（按新定义）是所有猛炸药的特性,炸药反应不充分并逐渐趋于充分是爆轰的增长的化学机制。     

弹黏塑性热点模型的冲击起爆临界条件

非均质炸药冲击起爆临界条件是武器传爆系列设计以及安全性能评估中十分关注的问题。基于Kim弹黏塑性热点模型,通过数值求解冲击波作用下炸药局部热点的温升模型,获得了TATB和HMX基炸药在不同冲击压力作用下的冲击起爆临界阈值,定量分析了孔隙度对炸药冲击起爆临界阈值的影响。与实验数据对比,结果表明:在1~10GPa范围内,采用该模型计算得到的冲击起爆临界阈值与一维短脉冲试验相符,对应的炸药冲击起爆临界阈值近似为一常量;当压力大于10GPa时,非均匀炸药的冲击起爆机制开始由局部热点机制向整体均匀加热机制转变;在一定压力范围内,炸药孔隙度越大,冲击起爆临界阈值越小。     

一种多孔铁的冲击压缩性

 用二级轻气炮作为动态加载装置,用电探针技术和阻滞法在80～160 GPa压力范围内测量了平均初始密度为6.904 g/cm³的多孔铁的冲击压缩性。实验结果表明,其冲击压缩线可以用D=2.977+1.603u_p的线性关系描述（D,u_p分别是冲击波速度和粒子速度,单位km/s）,这一结果与国外的实验结果和Wu-Jing模型的预测结果相符。     

BaCO3和TiO2粉末混合物冲击压缩性和BaTiO3冲击合成的实验研究

 利用高能炸药爆轰驱动冲击波、狭缝扫描闪光隙高速照相技术和阻抗匹配解原理，在10~100 GPa压力范围内，测量了BaCO₃和TiO₂粉末混合物的冲击绝热数据。同时，利用轴对称柱面和平面爆轰装置，进行了该混合物样品的冲击后回收实验和回收样品的X射线衍射分析，考察BaTiO₃的冲击合成。测量出的冲击绝热数据，以冲击波压力和比容平面上的结果为例，在约30和45 GPa两个压力值时，比容发生明显跃变。冲击绝热数据与回收样品X射线衍射分析结果相结合，判断出，这两个跃变分别对应于TiO₂从锐钛矿相转变到高压β-TiO₂相，BaCO₃与TiO₂开始急剧化学反应合成出BaTiO₃并放出CO₂。此外，在压力为10 GPa左右作回收实验，其回收样品的X射线衍射分析表明TiO₂由锐钛矿相完全转变为金红石相。     

凝聚炸药中超压爆轰的实验研究

 采用飞片碰撞技术，在TNT/RDX（40/60）炸药中获得了2.5倍于正常爆轰的最大超压值，得到了超压爆轰下爆轰产物物态方程p=Aρ^{k+A₁(p-p_J)}（p－爆压，单位GPa，ρ－密度，单位kg/m³，A=ρ_J/ρ^k_J，p_J=27.06 GPa，ρ_J=2.3×10³ kg/m³，k=2.77，A₁=2.7×10^-3 GPa^-1，下表J代表正常爆轰状态）。该方程还可以较好地描述超压爆轰产物的二次冲击状态。     

利用电磁法研究HMX与TATB混合钝感炸药的冲击起爆特性

为研究含有少量奥克托金(HMX)且以三氨基三硝基苯(TATB)为基的高能钝感炸药PBX-3的冲击起爆反应增长规律,采用火炮驱动蓝宝石飞片的方法和铝基组合式电磁粒子速度计技术进行了一维平面冲击实验。通过实验测量撞击表面及内部不同深度处的冲击波后粒子速度,得到PBX-3炸药的Hugoniot关系。根据冲击波示踪器所测数据绘制了炸药到爆轰的时间-距离(x-t)图,获得了反映炸药冲击起爆性能的Pop关系。将入射压力为12.964 GPa时达到爆轰的6条速度曲线修整成相同零点,通过读取6条曲线的分离点即反应区末端的C-J点,计算出化学反应区时间和宽度。     

JB-9001钝感炸药冲击Hugoniot关系测试

 利用“压力对比法”实验技术，通过锰铜压力计测试待测炸药样品和LY12铝样品在LY12铝飞片的同时撞击下的界面压力p_exp和p_Al，从冲击波关系式和正交回归直线拟合分析，确定了JB-9001钝感炸药的冲击Hugoniot关系。     

水绿矾的状态方程和高压熔化

 用阻抗匹配法和压电探针技术测量了初始密度为1.714 g/cm³（孔隙率α=ρ₀/ρ₀₀=1.898/1.714=1.107）的水绿矾（FeSO₄·7H₂O）的冲击压缩线,发现其在0～100 GPa范围内存在两个明显相区：含有部分熔融的低压相和完全熔化的高压相。在两个相区内,冲击波速度D和波后粒子速度u可分别描述为：D=0.59+2.06u（u<3.12 km/s）和D=3.18+1.223u（u≥3.12 km/s）。从冲击压缩数据出发,用欧拉有限应变理论得到了其等熵状态方程。其熔化方程可用p_m(GPa) =0.159(T_m(K)/1000)^6.3371+0.69来近似描述。     

爆轰产物物态方程及CHBr3相变的理论研究

 由吉布斯自由能最小计算处于化学平衡状态的气体和固体混合系统的平衡组分。以BKW和VLW作为爆轰产物的物态方程对几种炸药爆轰参数作了预言，计算结果与实验值吻合得非常好。另外，还对CHBr₃的冲击压缩分解作了化学平衡计算，给出了冲击压缩曲线，对文献[6]中提出的CHBr₃在55~60 GPa存在相变的看法提出了质疑。     

液态水、苯和壬基乳化剂混合物冲击压缩特性的实验研究

 利用二级轻气炮在3.75~57.87 GPa 压力范围内,对体积比为10∶10∶1的液态水-苯-壬基酚聚氧乙烯醚混合体系进行了动高压加载实验,获得了10个Hugoniot数据。拟合结果表明,该混合体系的D-u关系可近似用直线方程D=1.407+1.503u_p描述,拟合精度约为0.102。混合体系H₂O-C₆H₆-C₃₅H₆₄O₁₁的冲击压缩实验结果基本符合体积相加原理,而在给定的实验压力区间内,冲击绝热曲线发生多次拐折的事实意味着该系统可能在6 GPa、10 GPa和30 GPa压力点附近发生了多次结构性相变。另外,还讨论了Lawrence-Berthlot混合规则中修正因子对高密度条件下指数-6型相互作用势排斥部分的影响。     

Nonequilibrium Zeldovich-von Neumann-Doring theory and reactive flow modeling of detonation

This paper discusses the Nonequilibrium Zeldovich-von Neumann-Doring (NEZND) theory of self-sustaining detonation waves and the Ignition and Growth reactive flow model of shock initiation and detonation wave propagation in solid explosives. The NEZND theory identified the nonequilibrium excitation processes that precede and follow the exothermic decomposition of a large high explosive molecule into several small reaction product molecules. The thermal energy deposited by the leading shock wave must be distributed to the vibrational modes of the explosive molecule before chemical reactions can occur. The induction time for the onset of the initial endothermic reactions can be calculated using high pressure-high temperature transition state theory. Since the chemical energy is released well behind the leading shock front of a detonation wave, a physical mechanism is required for this chemical energy to reinforce the leading shock front and maintain its overall constant velocity. This mechanism is the amplification of pressure wavelets in the reaction zone by the process of de-excitation of the initially highly vibrationally excited reaction product molecules. This process leads to the development of the three-dimensional structure of detonation waves observed for all explosives. For practical predictions of shock initiation and detonation in hydrodynamic codes, phenomenological reactive flow models have been developed. The Ignition and Growth reactive flow model of shock initiation and detonation in solid explosives has been very successful in describing the overall flow measured by embedded gauges and laser interferometry. This reactive flow model uses pressure and compression dependent reaction rates, because time-resolved experimental temperature data is not yet available. Since all chemical reaction rates are ultimately controlled by temperature, the next generation of reactive flow models will use temperature dependent reaction rates. Progress on a statistical hot spot ignition and growth reactive flow model with multistep Arrhenius chemical reaction pathways is discussed. The text was submitted by the authors in English.     

Determination of detonation parameters of liquid high explosives

An experimental study of the detonation parameters and structure of the reaction zone for liquid high explosives (HEs), such as bis(2-fluoro-2,2-dinitroethyl)formal (FEFO), tetranitromethane (TNM), and nitromethane (NM) is performed. For each of these HEs, the time corresponding to the position of the Chapman-Jouguet point is determined: for FEFO, from experiments conducted at different charge diameters (≈300 ns); for TNM, at a fixed diameter but at different lengths (≈200 ns); and for NM, at the same diameter and length of the shell, but with detonation being initiated by different HE charge (≈50 ns). The particle velocity and pressure at the Chapman-Jouguet point for these explosives were measured. For TNM and NM, the dependence of the detonation velocity on the charge diameter was obtained     

Weak detonation in mixtures of phlegmatized RDX with aluminum

The Zel’dovich theory predicts the possibility of realization of self-sustained weak detonation in systems with nonmonotonic energy release. The present paper describes experiments aimed at detecting such a regime of detonation in mixtures of phlegmatized RDX with PP-1 and PAP-2 aluminum powders. The mass fraction of aluminum was 20%. To examine the detonation regimes, 70-mm-in-diameter charges of these mixtures were initiated with powerful triangular pressure pulses, which gave rise to attenuating overdriven detonation waves. The pressure profiles were recorded at various distances from the initiation plane (from 10 to 80 mm). Specific features of the time evolution of the detonation wave profile indicative of the existence of a supersonic flow region arising not later than 0.15 μs behind the shock front were revealed. The supersonic character of the flow behind an intermediate C-J plane is an inherent characteristic of self-sustained weak detonation; i.e., direct experimental evidence for the existence of weak detonation in RDX-aluminum mixtures was obtained.     

Review of the Forest fire model for high explosives

Forest fire is a burn model for reactive hydro simulations that is widely used to describe both initiation and propagation of detonation waves in solid high explosives. Here we thoroughly review the assumptions of the model. In analogy with Whitham–Chisnell shock dynamics, we derive the Forest fire rate based on a characteristic analysis of a shock-to-detonation transition. Code issues with implementing the Forest fire model are also discussed. The analysis leading to the Forest fire rate is more general than the simplifying assumptions used by the model. The Forest fire analysis provides important constraints needed for any burn model to fit shock initiation data. This data is fundamental to ignition sensitivity of high explosives.     

“闪光二号”电子束辐照平板靶产生热击波的实验研究

 热击波是电子束辐照靶材料时在其内产生材料响应的一个重要力学现象。论述了近两年来我们在“闪光二号”装置上进行电子束辐照平板靶产生热击波的实验研究。使用的靶厚为2.8~6.5 nm,靶材为LY-12铝,靶上能通量为87~152 J/cm²。实验结果表明,实测热击波应力峰值为0.35~2.0 GPa,热击波平均作用时间约为0.29 μs,均半高宽约为0.14 μs,平均上升时间约为0.10 μs。     

一维非定常炸轰的特征线方法数值模拟

本文用特征线方法计算了一维非定常炸轰的发展和传播问题。为模拟炸药的化学反应,采用了一种冲击波引爆的唯象模型。以PBX-9404高级炸药为例给出了计算的POP图与实验结果的比较以及不同时刻波后流场的分布。     

Initiation and propagation of detonation waves in combustible high speed flows

The initiation and propagation of detonation waves in combustible high speed flows were studied experimentally. A planar detonation wave traveling in an initiation tube was transmitted into a test section where a combustible high speed flow was induced by an incident shock wave generated in a shock tube. In this study, the flow Mach numbers were obtained as 0.9 and 1.2. The experimental results show that depending on the flow velocity, the apparent propagation velocity of a detonation wave is higher in the upstream and lower in the downstream direction than the CJ velocity. Smoked plate records reveal cellular patterns deformed in the flow direction, and the calculated aspect ratios of the cell were found to agree well with the experimental ones on the basis of the assumption that the velocity of the transverse wave is not affected by the flowing mixture. By analyzing the shock-wave diffraction at the position where there is an abrupt change in the area, on the basis of Whitham’s theory, it was deduced that in the present experimental set-up, the detonation was initiated by the reflection of the diffracted shock waves on the sidewalls of the test section. The agreement between the experimental and calculated results regarding the position of the cellular patterns on the smoked plate record indicated that the position of detonation initiation in high speed flows is shifted downstream due to the flow velocity.     

The mechanism of hot spot formation in condensed explosives

The hypothesis of an electrical mechanism of formation of detonation initiation zones (hot spots) in condensed explosives is considered. The hypothesis is based on the generation of electric fields and the appearance of shock-induced conductivity in the propagation of a shock wave (compression wave) in condensed dielectric media, including explosives. These physical phenomena can cause a local electrical breakdown, whose channel is identified with a hot spot. The available experimental data are analyzed from the point of view of the hypothesis suggested, and a procedure for verifying this hypothesis is outlined.     

Model of the spark discharge initiation of detonation in a mixture of hydrogen with oxygen

A model of the spark-discharge initiation of detonation was developed to integrally describe both spark channel processes and detonation initiation processes under the action of a spark-generated shock wave. The consumption of discharge energy for dissociation, ionization, and emission processes and conversion into thermal and kinetic energies with consideration for fuel combustion energy conversion was evaluated. The time history of the spark channel resistance was calculated. The time history of the fractions of energy inputted into a spark and lost for the heating of external circuits with respect to the total discharge energy was determined. Simulation was performed for capacitor discharge in a mixture of hydrogen with oxygen.