爆轰引爆过程中OH辐射的光谱研究

利用改进的大型棱镜谱仪的探测技术，研究了氢轰时引爆过程微秒量级ＯＨ辐射特性，为了解氢快速反应机理提供了定量结果。实验确定了ＯＨ辐射强度，感应时间与混合物寝压力的关系；富余的氢，氧对ＯＨ辐射的影响。     

利用火焰发射光谱来研究汽油机的燃烧过程

本文用一套精密的光电转换系统，采集了一台汽油机燃烧过程中火焰辐射在可见光到近紫外波段内的光谱，探测到了燃烧中间产物ＣＨ、ＣＮ、Ｃ２、Ｈ２Ｏ等的特征光谱，并分析了这些产物在燃烧过程中的变化规律，以及随过量空气系数，缸内压力的变化．实验结果表明，汽油机三个不同的燃烧阶段具有不同的燃烧光谱特征：着火过程中，存在着大量的处于激发态的分子、原子、离子、自由基等活化中心的束缚态光谱，随着燃烧发展，ＣＨ、Ｃ２自由基的光谱强度明显加强；当减小过量空气系数时，光谱强度变弱并且着火延迟期增长；自由基特征光谱的光强变化曲线可以反映它们在燃烧过程中的浓度变化．所以火焰发射光谱是实时检测燃烧中间产物，特别是ＣＨ、Ｃ２等有害排放物变化规律的有效手段，可以为分析、模拟燃烧过程，控制排放提供有用的实验数据．     

弱点火条件下炸药燃烧转爆轰的数值模拟

考察颗粒炸药从传导燃烧到对流燃烧再到爆轰的过程.对装填密度为85%的HMX颗粒炸药的燃烧转爆轰过程进行数值模拟,分析传导燃烧、对流燃烧和爆轰的发展过程.点火早期燃烧速度很低,火焰面在8.16 ms之内只前进了不到0.2 mm;形成对流燃烧之后燃烧速度快速增加,只用了0.1 ms就形成了速度为8 165 m·s^-1的稳定爆轰.当炸药颗粒直径或点火压力减小时,形成稳定爆轰所需的时间增加.     

起爆药爆轰场和燃烧场的干涉法显示及其图像处理

本文介绍了利用脉冲YAG激光引爆起爆药产生爆轰流场或燃烧温度场,用时间序列干涉法首次获得了爆轰流场和起始燃烧过程的时间序列干涉图的实验结果.在此基础上,采用条纹曲线检测法和双三次多结点插值样条函数从干涉图上提取爆轰场冲击波的波阵面,并通过序列波阵面配准算法,定量地计算了冲击波的传播速度.同时,还定量计算了燃烧场温度随时间变化的分布.     

炸药爆轰制备纳米石墨粉储放氢性能实验研究

介绍了一种新的制备纳米石墨粉的方法——炸药爆轰法.通过对爆轰合成的黑色粉末进行x射线衍射分析，确认其为六方结构的纳米石墨，平均晶粒度为1.86—2.61nm.用BET气体吸附仪测试纳米石墨粉的比表面积约为500—650m2/g，由比表面积计算得到的纳米石墨粒度为4.41—6.85nm.在室温（≈290K）和12MPa压力条件下对纳米石墨粉进行储放氢气性能测试，结果表明纳米石墨粉样品的储放氢量为0.33wt%—0.37wt％.在相同实验条件下，纳米石墨粉原始样品的储放氢能力较原始纳米炭纤维（0.15wt%—0.35wt％）和多壁碳纳米管（0.15wt%—0.20wt％）的储放氢能力略强,但低于超级活性炭（0.92wt%—0.98wt％）.纳米碳材料的比表面积在其储放氢实验中起关键作用. 关键词： 爆轰 纳米石墨粉 比表面积 储放氢量     

以HMX为基的两种压装高密度炸药的燃烧转爆轰实验研究

 为研究以HMX为基的固体高能炸药的燃烧转爆轰性能,采用同轴电探针和压力传感器测试技术对常用的A、B两种压装高密度高能炸药开展燃烧转爆轰实验,研究装药组分和约束条件对压装高密度炸药燃烧转爆轰性能的影响。实验结果表明：这两种压装高密度炸药难以发生燃烧转爆轰;在强约束条件下（45号钢,内径25.4 mm、外径65 mm、长度600 mm）,A压装炸药（HMX质量分数为95%,密度为1.86 g/cm³）基本实现了燃烧转爆轰,爆轰诱导距离约为545 mm;在相同的实验条件下,A压装炸药比B压装炸药（HMX质量分数为87%,密度为1.84 g/cm³）更易于发生燃烧转爆轰,即A压装炸药的安定性相对较差。     

DDT管材料对颗粒状RDX床燃烧转爆轰（DDT）影响的实验研究

 采用盖帽探针、离子探针实验研究了点火药点燃时,DDT管材料变化（钢和铝）对颗粒状RDX床的燃烧转爆轰的影响。     

利用OMA谱仪测量飞秒激光的谐波光谱

本文给出了利用光学多道分析(OMA)谱仪测量飞秒激光谐波光谱的一种方法 .该方法是利用OMA谱仪(谱分辨0.1nm)加CCD(1152×1242)相机探测设备,用消色差的相机镜头作为空间分辨,在固体靶前表面测量了激光的二次谐波(2ω_0)光谱.结果显示:在平行于靶面的方向和接近于法线方向分别观测到了2ω_0光谱,但在接近于法线方向的谐波光谱出现了精细结构,并得到2ω_0谐波谱的分裂间隔约为3.183 nm.分析认为,自生磁场的产生和作用是导致二次谐波光谱精细结构及谐波谱分裂的主要原因.     

爆轰作用下激波管壁发射光谱的研究

 本文用KODAK-2485胶片拍摄了激波管内四种烃燃料（正庚烷、异辛烷、M-17乳化汽油、W-11乳化汽油）的爆轰光谱。发射光谱由爆轰产物产生的连续光谱，Fe、Cr、Mn原子的大量线光谱，以及550~660 nm强而复杂的带光谱组成。经分析，在这些带光谱中存在FeO分子的黄带系光谱。     

高密度B炸药的燃烧转爆轰实验

在相同的实验条件下研究了3种不同密度固体压装B炸药（TNT，RDX为40／60）的燃烧转爆轰性能。3种B炸药的密度分别为1．597，1．654g／cm^3与1．681g／cm^3。用时间间隔记录仪、电离式电探针系统记录燃烧波、压缩波或爆轰波到达的时间；用程控电荷放大器、数字示波器及压力传感器记录DDT管不同位置处的压力历程。起爆器、时间间隔记录仪及示波器均由同步机触发。DDT管材料为45号钢，内径φ20mm，外径φ64mm，长度500mm；点火药为小粒黑，质量1．1～1．2g；所使用的电探针为同轴电探针（芯线为0．9mm的铜漆包线，     

An experimental investigation of the propagation mechanism of critical deflagration waves that lead to the onset of detonation

The reflection of a CJ detonation from a perforated plate is used to generate high speed deflagrations downstream in order to investigate the critical conditions that lead to the onset of detonation. Different perforated plates were used to control the turbulence in the downstream deflagration waves. Streak Schlieren photography, ionization probes and pressure transducers are used to monitor the flow field and the transition to detonation. Stoichiometric mixtures of acetylene–oxygen and propane–oxygen were tested at low initial pressures. In some cases, acetylene–oxygen was diluted with 80% argon in order to render the mixture more “stable” (i.e., more regular detonation cell structure). The results show that prior to successful detonation initiation, a deflagration is formed that propagates at about half the CJ detonation velocity of the mixture. This “critical” deflagration (which propagates at a relatively constant velocity for a certain duration prior to the onset of detonation) is comprised of a leading shock wave followed by an extended turbulent reaction zone. The critical deflagration speed is not dependent on the turbulence characteristics of the perforated plate but rather on the energetics of the mixture like a CJ detonation (i.e., the deflagration front is driven by the expansion of the combustion products). Hence, the critical deflagration is identified as a CJ deflagration. The high intensity turbulence that is required to sustain its propagation is maintained via chemical instabilities in the reaction zone due to the coupling of pressure fluctuations with the energy release. Therefore, in “unstable” mixtures, critical deflagrations can be supported for long durations, whereas in “stable” mixtures, deflagrations decay as the initial plate generated turbulence decays. The eventual onset of detonation is postulated to be a result of the amplification of pressure waves (i.e., turbulence) that leads to the formation of local explosion centers via the SWACER mechanism during the pre-detonation period.     

On the transition from deflagration to detonation

Feedback between the turbulent-flow and deflagration-wave parameters leads to breakage of the combustion regime. Critical conditions of the development of this instability are formulated.     

小型棱镜摄谱仪的应用

利用小型棱镜摄谱仪看谱系统对汞光谱进行谱线的测量,给出较为完整的汞光谱,使学生在实验中有较为明确的依据.     

Critical deflagration waves leading to detonation onset under different boundary conditions

High-speed turbulent critical deflagration waves before detonation onset in H2–air mixture propagated into a square cross section channel,which was assembled of optional rigid rough,rigid smooth,or flexible walls.The corresponding propagation characteristic and the influence of the wall boundaries on the propagation were investigated via high-speed shadowgraph and a high-frequency pressure sampling system.As a comprehensive supplement to the different walls effect investigation,the effect of porous absorbing walls on the detonation propagation was also investigated via smoke foils and the high-frequency pressure sampling system.Results are as follows.In the critical deflagration stage,the leading shock and the closely following turbulent flame front travel at a speed of nearly half the CJ detonation velocity.In the preheated zone,a zonary flame arises from the overlapping part of the boundary layer and the pressure waves,and then merges into the mainstream flame.Among these wall boundary conditions,the rigid rough wall plays a most positive role in the formation of the zonary flame and thus accelerates the transition of the deflagration to detonation(DDT),which is due to the boost of the boundary layer growth and the pressure wave reflection.Even though the flexible wall is not conducive to the pressure wave reflection,it brings out a faster boundary layer growth,which plays a more significant role in the zonary flame formation.Additionally,the porous absorbing wall absorbs the transverse wave and yields detonation decay and velocity deficit.After the absorbing wall,below some low initial pressure conditions,no re-initiation occurs and the deflagration propagates in critical deflagration for a relatively long distance.     

Phase transition rate of anatase during detonation synthesis of TiO2

TiO₂ powders were synthesized by two types of mixed explosives in a sealed reaction kettle. The phase and morphology of TiO₂ powders were obtained by X-ray diffractometry and transmission electron microscopy. Results indicate that powders obtained from metatitanic acid contained mixed explosive are mixed crystal of anatase and rutile. The phase transition rate of anatase increases from 22.9% to 93.3% with the rise of mass ratio of hexogen, and the grain size also enlarges gradually. The powder obtained from anatase contained mixed explosive is rutile, and the phase transition rate of anatase is 100%. Compared with that before detonation, the grain size of anatase after detonation significantly changes, from nanoscale to micronscale. Based on the calculation of detonation parameters, the phase transition process and grain growth during the synthesis of TiO₂ by means of detonation method are analyzed, and the nucleating collision–growth model is proposed.     

The effects of flame generated turbulence for turbulent-induced deflagration to detonation transition

The turbulent deflagration to detonation transition (DDT) process occurs when a subsonic flame interacts with intense turbulence resulting in spontaneous acceleration and the onset of DDT. The mechanisms that govern the spontaneous ignition are deduced intricately in numerical simulations. This work experimentally explores the conditions that are known precursors to detonation initiation. More specifically, the experiment presented investigates the role of flame-generated compression as a cycle that continuously amplifies until a hotspot forms on the flame front and ignites. The study quantifies the compression comparatively against other flame regimes through ultra-high speed pressure measurements while qualitatively detailing flame generated compression through density gradients via schlieren imaging. Additionally, flow field measurements are quantified throughout the flow using simultaneous particle image velocimetry (PIV) and OH* chemiluminescence. The turbulence fluctuations and flame speeds are extracted from these measurements to identify the reactant conditions where flame-generated compression begins. Collectively, these simultaneous high-speed measurements provide detailed insight into the flame and flow field characteristics where the runaway process occurs. This work ultimately documents direct flow field measurements to extract the contribution of flame-generated turbulence on the turbulent deflagration to detonation transition process.     

Influence of chemical kinetics on spontaneous waves and detonation initiation in highly reactive and low reactive mixtures

Understanding the mechanisms of explosions is important for minimising devastating hazards. Due to the complexity of real chemistry, a single-step reaction mechanism is usually used for theoretical and numerical studies. The purpose of this study is to look more deeply into the influence of chemistry on detonation initiated by a spontaneous wave. The results of high-resolution simulations performed for one-step models are compared with simulations for detailed chemical models for highly reactive and low reactive mixtures. The calculated induction times for H₂/air and for CH₄/air are validated against experimental measurements for a wide range of temperatures and pressures. It is found that the requirements in terms of temperature and size of the hot spots, which can produce a spontaneous wave capable to initiate detonation, are quantitatively and qualitatively different for one-step models compared to detailed chemical models. The time and locations when the exothermic reaction affects the coupling between the pressure wave and spontaneous wave are considerably different for a one-step and detailed models. The temperature gradients capable to produce detonation and the corresponding size of hot spots are much shallower and, correspondingly, larger than those predicted using one-step models. The impact of the detailed chemical model is particularly pronounced for the methane-air mixture. In this case, not only the hot spot size is much greater than that predicted by a one-step model, but even at the elevated pressure, the initiation of detonation by a temperature gradient is possible only if the temperature outside the gradient is rather high, so that can ignite a thermal explosion. The obtained results suggest that the one-step models do not reproduce correctly the transient and ignition processes, so that interpretation of the simulations performed using a one-step model for understanding mechanisms of flame acceleration, DDT and the origin of explosions must be considered with great caution.     

Effects of heat loss and viscosity friction at walls on flame acceleration and deflagration to detonation transition

The coupled effect of wall heat loss and viscosity friction on flame propagation and deflagration to detonation transition(DDT) in micro-scale channel is investigated by high-resolution numerical simulations.The results show that when the heat loss at walls is considered, the oscillating flame presents a reciprocating motion of the flame front.The channel width and Boit number are varied to understand the effect of heat loss on the oscillating flame and DDT.It is found that the oscillating propagation is determined by the competition between wall heat loss and viscous friction.The flame retreat is led by the adverse pressure gradient caused by thermal contraction, while it is inhibited by the viscous effects of wall friction and flame boundary layer.The adverse pressure gradient formed in front of a flame, caused by the heat loss and thermal contraction, is the main reason for the flame retreat.Furthermore, the oscillating flame can develop to a detonation due to the pressure rise by thermal expansion and wall friction.The transition to detonation depends non-monotonically on the channel width.     

Numerical studies on autoignition and detonation development from a hot spot in hydrogen/air mixtures

Detonation development inside spark ignition engines can result in the so called super-knock with extremely high pressure oscillation above 200?atm. In this study, numerical simulations of autoignitive reaction front propagation in hydrogen/air mixtures are conducted and the detonation development regime is investigated. A hot spot with linear temperature distribution is used to induce autoignitive reaction front propagation. With the change of temperature gradient or hot spot size, three typical autoignition reaction front modes are identified: supersonic reaction front; detonation development and subsonic reaction front. The effects of initial pressure, initial temperature, fuel type and equivalence ratio on detonation development regime are examined. It is found that the detonation development regime strongly depends on mixture composition (fuel and equivalence ratio) and thermal conditions (initial pressure and temperature). Therefore, to achieve the quantitative prediction of super-knock in engines, we need use the detonation development regime for specific fuel at specific initial temperature, initial pressure, and equivalence ratio.     

Flame acceleration and the transition to detonation of stoichiometric ethylene/oxygen in microscale tubes

Flame propagation in capillary tubes with smooth circular cross-sections and diameters of 0.5, 1.0, and 2.0 mm are investigated using high-speed photography. Flames were found to propagate and accelerate to detonation speed in stoichiometric ethylene and oxygen mixtures initially at room temperature in all three tube diameters. Ignition occurs at the midpoint along the length of the tube. We observe for the first time transition to detonation in micro-tubes. Detonation was observed with both spark and hot-wire ignition. Tubes with larger diameters take longer to transition to detonation. In fact, transition distance scales with the diameter in our 1.0 and 2.0 mm cases with spark ignition. Flame structures are observed for various stages of the process. Three types of flame propagation modes were observed in the 0.5 mm tube with spark ignition: (a) acceleration to Chapman–Jouguet (CJ) detonation speed followed by constant CJ wave propagation, (b) acceleration to CJ speed, followed by the detonation wave failure, and (c) flame acceleration to a constant speed below the CJ speed of approximately 1600 m/s. The current detonation mechanism observed in capillary tubes is applicable to predetonators for pulsed detonation, micro propulsion devices, safety issues, and addresses fundamental issues raised by recent theoretical and numerical analyses.