氢氧爆轰波在激波管中的成长机制研究

 针对气相爆轰波成长机制研究,采用压力传感器和高速摄影技术,测试了氢氧混合气体在点火后的火焰波、前驱冲击波以及爆轰波的成长变化过程,计算了冲击波过程参数和气体状态参数,分析了火焰加速机制。实验结果表明,APX-RS型高速摄影系统可用于拍摄气相爆轰波的成长历程;氢氧爆轰波的产生是由于湍流火焰和冲击波的相互正反馈作用,导致反应区内多处发生局部爆炸,爆炸波与冲击波相互耦合,最终成长为定常爆轰波。     

气相DDT中过爆轰现象产生条件的实验研究

针对目前国际上关于气相过爆轰产生条件的3种不同观点,利用压力传感器,实验研究了氢氧混合物的爆燃转爆轰(DDT)全过程。获得了比较完整的、能反映气相DDT从爆燃成长为过爆轰再衰减为稳定爆轰的全过程压力变化曲线。分析实验结果表明,氢氧混合物的DDT过程中,过爆轰的产生需要一定条件;在初始压力一定的情况下,氢氧混合物DDT过程的转变时间或距离随氢气浓度的增加,先减小后增大,过爆轰的压力峰值约为稳定爆轰压力的1.5～2倍。     

激光支持等离子体爆轰波温度的实验测量

 高能量激光聚焦空气产生等离子体,等离子体进一步吸收激光能量会形成激光支持等离子体爆轰波。等离子体爆轰波温度是表征爆轰波的一个重要参数,研究等离子体爆轰波温度对于深入了解激光支持等离子体爆轰波形成机理有重要意义。分析了激光聚焦空气形成等离子体爆轰波过程和影响等离子体爆轰波温度的主要因素。采用多通道瞬态光学高温计,测量了不同激光发射能量下空气中形成的激光支持等离子体爆轰波的辐射强度,获得了一系列等离子体爆轰波温度动态变化曲线。测量结果表明：等离子爆轰波温度在随时间演化过程中出现3个峰,最高温度在7 000～10 000 K范围内;激光能量与等离子体爆轰波温度没有明显的相关性。     

纳米二氧化钛粉体的气相爆轰制备

 介绍了利用氢氧混合气体为原料、以四氯化钛为前驱体、气相爆轰制备纳米二氧化钛粉体的方法。利用XRD衍射结果分析证明，产物为金红石相和锐钛矿相的二氧化钛混晶，其晶粒尺度为纳米量级。通过XRD、SEM、TEM分析可以得出，粒子基本为球形，大部分粒子粒径为10~20 nm，也有少量的100 nm左右的粒子产生。分析后发现，反应发生在爆燃转爆轰的过程中和爆轰管中的湍流现象是导致大粒子产生的主要原因。在对在氢过量和氧过量两种状况下，对爆轰所产生的产物的形貌进行了对比，分析发现两种状况产生纳米二氧化钛粉末粒径分布和形貌并没有太大变化。     

炸药爆轰瞬态温度的光谱法测定

在双谱线原子发射光谱测温原理的基础上,设计了对炸药爆轰的瞬态温度进行实时测量的光纤光谱测试系统,利用光学纤维将炸药爆轰的光谱信号传入测光系统,用多通道数据采集器处理数据,系统的时间分辨率可高达0.1μs,所选择的两条谱线的波长分别为CuI 510.5和CuI 521.8nm,为炸药爆温的测量提供了一种简单有效的方法。利用该测温系统,通过对炸药爆轰光谱的测量,获得了实时瞬态爆轰温度-时间分布曲线。     

化学反应和球面聚心爆轰波的相互作用

考察球面爆轰波聚心传播过程中,波阵面附近压力和温度不断升高引起化学反应进程的改变;对比氢氧可燃气体与氮气的数值模拟结果,分析化学反应对波面温度和压力的影响,从而考察Zeldovich理论预测聚心爆轰波后参数的精确性.数值结果表明,爆轰波聚心传播初期,放热的燃烧反应对波后热力学参数起主导作用;传播后期,波阵面趋近于对称中心时,吸热的气体解离反应变得非常活跃,解离反应对后期的汇聚压力影响不大,但会在很大程度上限制汇聚温度的升高.     

战斗部爆轰产物温度效应数值模拟

 利用BKW代码、JWL方程和LS-DYNA程序，研究了无约束、弱约束和强约束等三种战斗部约束条件下炸药爆轰产物密度随时间的变化关系，再结合爆轰产物HOM状态方程获得爆轰产物温度随时间的衰变函数。给出了战斗部爆轰产物温度的理论计算方法。研究表明，爆轰区内爆轰产物温度及其衰减速率并不均匀，战斗部炸药的约束条件对爆轰产物密度和温度有重要影响，强约束可以延缓爆轰产物密度和温度的衰减，相同情况下仅战斗部壳体厚度加倍并不会导致爆轰产物密度和温度的衰减情况同比例变化。     

测量冲击温度的六通道瞬态光学高温计

 研制了一台测量冲击载荷下材料光谱辐射的瞬态光学高温计。在可见光和近红外光谱范围内，把光源的热辐射取出六个波段进行测量。每个波段信号通过各自的光线传输，光电倍增管探测和示波器记录。系统的时间分辨率约为20 ns。冲击温度测量范围为2 400~9 000 K，测量误差小于3%。给出了以空气和NaI警惕为样品的若干爆轰实验结果。     

无氧铜冲击熔化温度的辐射法测量

 在发生冲击熔化的情况下，金属样品/窗口界面压力下的熔化温度与卸载温度数值相等，且十分接近于界面温度值。根据这一结论，利用二级轻气炮加载手段和光辐射法测温技术，用氟化锂（LiF）单晶作透明窗口，获得了110~140 GPa压力范围内无氧铜的熔化温度。实验表明，无氧铜的高压熔化温度数据与文献发表的无氧铜高压声速实验结果是一致的，铜的高压熔化规律可用Lindemann熔化定律近似描述。采用的熔化温度测量方法不必反演出冲击温度，简化了冲击熔化温度的数据处理方法，为金属冲击熔化温度测量提供了一种潜在的技术途径。     

一维过驱动爆轰波形成的数值研究

利用有限速率的基元反应模型对一维过驱动爆轰波的形成过程进行数值模拟.研究表明,在上游高温、高压、高速来流作用下首先会形成一道强激波,其波面方存在诱导区和放热区,然后诱导区和放热区界面会在来流扰动的作用下发生失稳,经过复杂的波系运动过程形成过驱动爆轰波.通过对不同初始条件下界面失稳过程的模拟和分析,研究了混合气体的组元、温度,来流的压力、温度、速度对过驱动爆轰波形成的影响.     

On detonation initiation by a temperature gradient for a detailed chemical reaction models

The evolution from a temperature gradient to a detonation is investigated for combustion mixture whose chemistry is governed by a detailed chemical kinetics. We show that a detailed chemical reaction model has a profound effect on the spontaneous wave concept for detonation initiation by a gradient of reactivity. The evolution to detonation due to a temperature gradient is considered for hydrogen-oxygen and hydrogen-air mixtures at different initial pressures. It is shown that the minimal length of the temperature gradient for which a detonation can be ignited is much larger than that predicted from a one-step chemical model.     

Parametric scattering of high-frequency elastic waves by a small spherical cavity oscillating under the action of a Rayleigh wave

Scattering of high-frequency transverse and longitudinal plane waves incident on a spherical cavity located at a small depth under the surface of a half-space is considered. The cavity oscillates as a whole in the field of a low-frequency Rayleigh surface wave, the oscillation vectors of the longitudinal, transverse, and surface waves being coplanar. The cavity radius is assumed to be small compared to the wavelengths of the sounding wave and the pumping surface wave. The scattered compression and shear waves at the combination frequencies ω±Ω are calculated in the dipole approximation. Expressions obtained describe the qualitative behavior of the combination-frequency signal levels produced at the outputs of horizontally and vertically oriented geophones moving over the free surface of the elastic half-space.     

Detonation simulations in supersonic flow under circumstances of injection and mixing

The unsteady, reactive Navier-Stokes equations with a detailed chemical mechanism of 11 species and 27 steps were employed to simulate the mixing, flame acceleration and deflagration-to-detonation transition (DDT) triggered by transverse jet obstacles. Results show that multiple transverse jet obstacles ejecting into the chamber can be used to activate DDT. But the occurrence of DDT is tremendously difficult in a non-uniform supersonic mixture so that it required several groups of transverse jets with increasing stagnation pressure. The jets introduce flow turbulence and produce oblique and bow shock waves even in an inhomogeneous supersonic mixture. The DDT is enhanced by multiple explosion points that are generated by the intense shock wave focusing of the leading flame front. It is found that the partial detonation front decouples into shock and flame, which is mainly caused by the fuel deficiency, nevertheless the decoupled shock wave is strong enough to reignite the mixture to detonation conditions. The resulting transverse wave leads to further mixing and burning of the downstream non-equilibrium chemical reaction, resulting in a high combustion temperature and intense flow instabilities. Additionally, the longitudinal and transverse gradients of the non-uniform supersonic mixture induce highly dynamic behaviors with sudden propagation speed increase and detonation front instabilities.     

Detonation propagation across a stratified layer with a diffuse interface

A study was conducted to examine detonation propagation in a stratified layer of hydrogen-oxygen-nitrogen above an inert gas in a horizontal narrow channel. The stratified layer was produced by a gravity current, generated by retracting a door initially separating a hydrogen-oxygen-nitrogen mixture in the predetonator and a heavier inert gas in the test-section. A steady detonation wave generated in the predetonator was transmitted into the stratified layer. The reactivity of the predetonator mixture was varied via the hydrogen-oxygen equivalence ratio and the amount of nitrogen dilution. Schlieren photography was used to visualize the detonation front in the test-section, and soot foils were used to obtain the cellular structure. Schlieren imaging showed a curved detonation front that decoupled at about mid channel height, into a shock wave and trailing contact surface. Both the hydrogen-oxygen-nitrogen reactivity and the type of inert gas initially in the test-section affected the distance travelled by the detonation wave in the stratified layer. The mixture composition distribution within the test-section before ignition was obtained via a three-dimensional CFD simulation. The lateral extent of the cellular structure captured on the soot foil, coincided with the calculated inert gas mole fraction contour that corresponds to a sharp increase in the ZND induction zone length, e.g., 70% argon dilution for a stoichiometric hydrogen-oxygen predetonator mixture.     

Numerical study of three-dimensional detonation wave dynamics in a circular tube

The three-dimensional structures of a detonation wave propagating in a circular tube were investigated using a one-step irreversible Arrhenius kinetics model. A series of parametric studies were carried out to investigate the different modes of cell structure formation by changing the pre-exponential factor. Maximum pressure trace was recorded along the tube wall to investigate the detonation cell structures. The unsteady results obtained in three dimensions revealed the generation mechanism of the wave front structures of two-, three- and four-cell mode detonations. A six-cell mode detonation could be obtained using a finer grid. With the increase in pre-exponential factor, it was found that the number of detonation cells is increased while the cell size is reduced accordingly. In all the multi-cell modes, the detonation wave structures and smoked-foil records on the wall are formed by the propagation of transverse waves along the wall in clockwise and counter-clockwise directions, while the slapping wave moves in the radial direction. The presence of the slapping wave further strengthens the wave interactions in three-dimensional simulation. Comparison with two-dimensional simulation confirms the effect of the slapping wave in the radial direction. As a result, the detonation wave front structures changes from the polygonal shape to the multi-bladed fan shape, periodically.     

Wave spectra in solid and liquid complex (dusty) plasmas

Spectra of longitudinal and transverse waves were obtained experimentally in liquid and solid two-dimensional complex (dusty) plasmas at different kinetic temperatures. As the temperature increased and the phase state of the plasma changed from solid to liquid, the phonon spectra of both longitudinal and transverse modes broadened (especially at high wave numbers), indicating increased damping. The transverse mode disappeared and a thermal (compressional) mode appeared.     

Three-dimensional detonation structure and its response to confinement

Three-dimensional (3D) detonation simulations solving the compressible Navier-Stokes equations with detailed chemistry are performed in both square channel and round tube geometries. The simulations are compared with each other and with two-dimensional (2D) channel simulations and round tube experiments of identical mixture and conditions (stoichiometric hydrogen-oxygen with 3000 PPMv ozone at 300 K and 15 kPa) with the goal of understanding the effect of confinement and boundaries on detonation structure. Results show that 3D detonations propagate with highly inhomogeneous blast dynamics, where blasts emerge not only from intersections of two transverse waves (similar to 2D propagation) but also from intersections of many transverse waves (unique to 3D detonations in the confinements tested). Intersections of many transverse waves lead to extreme thermodynamic states and highly overdriven wave velocities, well in excess of those seen in the ZND model and in 2D simulations. 3D simulations in the square tube show highly regular blast latticing, smaller detonation cells, and highly oscillatory velocities when compared to the round tube simulations. Round tube simulations show more spatially non-uniform blast dynamics. The conclusions reached in the current work are found irrespective of numerical grid resolution.     

Initiation of a detonation wave by resonant laser radiation in a hydrogen-oxygen mixture flowing about a wedge

The formation of an oblique detonation wave in a supersonic hydrogen-oxygen flow about a planar wedge is considered. It is shown that the excitation of the electronic state b ¹Σ _g ⁺ in oxygen molecules by resonant laser radiation with a wavelength of 762 nm makes it possible to initiate detonation combustion at a distance of ≈1 m from the tip of the wedge at low temperatures (500–600 K). Notably, it suffices to irradiate the gas in the narrow (0.5–1.0 cm across) paraxial region of the flow near the tip of the wedge. It is found that the laser-induced excitation of molecular oxygen is several times more efficient than ordinary heating of the mixture to initiate a detonation wave.     

瞬时多光谱爆温测量系统

本文针对国内外近年来常用的爆炸温度测量方法在原理、结构上的不足,提出了一种更符合实际测量要求的瞬时多光谱爆温测量系统,阐述了它的基本工作原理,给出了总体构成结构,并指出了这种新方案不同于以往方法的特点.利用该系统可在一次爆炸过程的100ns时间内完成四个时刻爆轰温度的测量,最后通过阶段实验结果证实了它的可行性.