Experimental and numerical studies of underwater shock wave attenuation

The attenuation of an underwater shock wave by a thin porous layer is studied both experimentally and numerically. The shock waves are generated by exploding 10 mg silver azide pellets and the pressures at different distances from the explosion center are measured. Measurements are also carried out with a gauze layer placed between the explosion source and the pressure gauge. The results with and without the gauze layer are compared evaluating the shock wave attenuation. Numerical simulations of the phenomenon are also carried out for a simple wave attenuation model. The results are compared with the experimental data. Despite the simple mathematical model of wave attenuation, the agreement between the experimental and numerical results is reasonable.Received: 22 October 2002, Accepted: 17 June 2003, Published online: 5 August 2003PACS: 47.11.+j, 47.40.Nm, 47.55.Mh     

一种三阶有限体积法及其在欠膨胀射流激波结构数值模拟中的应用

以喷管出口欠膨胀射流为研究对象,在Lagrange坐标系下建立欠膨胀射流二维积分形式的流动方程。通过在单元交接面处进行三阶ENO(essentially nonoscillatory)格式插值,构造得到一种适用于求解该方程的三阶ENO有限体积法。采用该格式对一维Sod激波管算例和喷管出口欠膨胀射流进行数值计算。计算结果表明,该方法具有高精度、基本无振荡的特点,能很好地捕捉包含激波、滑移线以及三波交点等复杂流场波系结构。计算得到的波系结构中马赫盘的位置与实验结果吻合很好,相对误差小于1.1%。     

Modeling jet flows caused by the incidence of a shock wave on a profiled free surface

The problem of the incidence of a shock wave with a front-pressure amplitude of about 30 GPa at the profiled free surface of an aluminum sample is studied. It is shown that in the case of large perturbations (amplitude 1 mm and wavelength 10 mm), jet flows occur on the free surface. The data obtained are described using a kinetic fracture model that takes into account the damage initiation and growth in the material due to tensile stress and shear strain. __________ Translated from Prikladnaya Mekhanika i Tekhnicheskaya Fizika, Vol. 48, No. 1, pp. 16–23, January–February, 2007.     

液滴对爆炸冲击波的衰减作用

为分析液滴对舰船舱内爆炸冲击波的耗散与衰减作用,通过有限元分析方法,建立冲击波作用于不同尺寸单个液滴和多排液滴的模型,分析冲击波与单个及多个液滴的作用过程及液滴形态变化,对冲击波衰减规律进行分析总结。得到结论如下:单个液滴模型中,小液滴破碎更迅速,破碎的规律性强;大液滴抛撒现象发生较早,抛撒出的小液滴数目多,但整体变化规律性偏差;不同尺寸单个液滴对冲击波有一定的衰减作用,衰减率随液滴尺寸增大而增大,线性规律较明显;成排液滴对冲击波有明显的衰减作用,相同液滴密度下衰减率随着液滴数量的增多而增大,呈现明显的线性特性。     

水下连续脉冲冲击波的声学特性

为探求金属爆炸索在水下爆炸声源研究领域的应用前景,设计了一种可以连续产生若干个脉冲冲击波的装置,称之为水下连续脉冲冲击波发生装置。利用小波分析对该装置产生的连续脉冲冲击波信号进行分解与重构,考察其频谱特性,并进一步分析了信号的声压级特性。结果表明：该装置产生的信号声压级较高,具有很强的声功率;信号包含频率十分丰富,雷管和金属爆炸索由于装药结构及传爆方式的不同,爆炸所产生的冲击波频谱特性也有所差异。雷管爆炸产生的冲击波主要分布在15.6 kHz以下的频带内,金属爆炸索爆炸产生的脉冲冲击波信号则主要分布在62.5 kHz以下的频带内;脉冲冲击波的个数和声持续时间可由爆炸索的排列方式和长度控制,脉冲冲击波间的时间间隔可调,发生装置稳定易控     

Instability theory of shock wave in a channel

The instability theory of shock wave was extended from the case with an infinitefront to the case of a channel with a rectangular cross section.First,themathematical formulation of the problem was given which included a system ofdisturbed equations and three kinds of boundary conditions.Then,the general solutionsof the equations upstream and downstream were given and each contained fiveconstants to be determined.Thirdly,under one boundary condition and oneassumption,it was proved that all of the disturbances in front of the shock front andone of the two acoustic disturbances behind the shock front should be zero.Theboundary condition was that all of the disturbed physical quantities should approach tozero at infinity.The assumption was that only the unstable shock wave was concernedhere.So it was reasonable to assumeω=iγ,γwas the instability growth rate andwas a positive real number.Another kind of boundary conditions was that the normaldisturbed velocities should be zero at the solid wall of the cha     

Instability theory of shock wave in a shock tube

The instability theory of shock wave in a shock tube including the effects of tube wall and contact surface is studied. The experimental data of unstable shock wave coincide with one of instability criteria derived in the present paper.     

水中冲击波与弹性薄板耦合作用的研究

对水中冲击波与弹性薄板的流固耦合作用进行了研究,建立了实验装置。利用全息干涉法定量测量了水中动态流场,并测出受水中冲击波作用的弹性薄板在不同时刻的变形,得出相应的全息干涉条纹图。同时利用有限元法对水中冲击波与弹性薄板的流固耦合问题进行了数值计算。研究结果表明,用实验方法能够较好地模拟水中冲击波与弹性结构的耦合作用,用有限元法计算水中冲击波传播问题是可行的。     

锥形长药柱水下爆炸冲击波参数计算方法

为了计算锥形长药柱水下爆炸冲击波压力,以及研究长脉宽冲击波的传输特性,基于叠加原理建立了冲击波压力-时间曲线的计算方法,通过实验验证了该方法的有效性,在此基础上分析了锥形长药柱不同方位冲击波压力的分布规律。研究结果表明:锥形长药柱产生的冲击波压力具有各向异性,在起爆端一侧形成的是具有厚波头特征的低幅值长脉宽冲击波,在装药径向形成的是接近指数衰减的高幅值冲击波,而在远离起爆端的冲击波压力幅值和脉宽则介于前两者之间。锥形长药柱与球形装药冲击波分布的差异是由于装药形状和起爆方式的改变所导致的,由于装药不同部位起爆的时间差,导致水下爆炸冲击波在不同位置的叠加效果存在明显差异,药柱周围流场中形成的冲击波压力具有方向性。利用提出的计算方法得到的计算结果与实验结果和数值模拟结果吻合较好,研究结果可为锥形长药柱水下爆炸冲击波威力场和毁伤评估提供参考和依据。     

冲击波作用下乳化炸药压力减敏的表征方法

引入一个新的物理量压力减敏程度,来更合理地表征乳化炸药发生压力减敏的难易程度,为研究其作用机理提供量化的分析工具。分别利用乳化炸药发生压力减敏前后的爆炸冲击波峰压及其对数、冲击波能量和总能量计算压力减敏程度,比较并分析计算结果的优劣。结果表明,几个参数计算的结果都能达到相近的效果,用冲击波峰压计算起来简单方便,冲击波能量计算效果较好。用冲击波参数计算的压力减敏程度能够反映乳化炸药压力减敏的本质,建议采用冲击波峰压计算压力减敏程度,在数值差别不明显时采用冲击波能量来计算。     

水下爆炸冲击波载荷作用下冰层破碎特性及其影响因素

水下爆炸破冰是复杂的爆破工程,为了研究冰层在水下爆炸冲击波载荷作用下的破碎特性及规律,利用几何动力分析软件LS-DYNA对水下爆炸破冰的过程进行数值模拟,并将计算结果与实验结果进行对比,误差在8%以内,验证了数值模型的有效性。根据本文中的建模方法及建立的模型,计算不同的实验工况:实验场地环境不变,调整爆距分析不同爆距下冰层破碎特性;调整药量、爆距和冰厚,通过正交设计方法设计9组实验方案,应用灰色系统理论对3种因素进行分析,建立了各个因素与破冰半径之间的灰色关联度系数及灰色关联度。分析结果表明:药量为100 g,冰厚为29 cm,水深为2.9 m,爆距范围为0.3~1.5 m破冰的半径范围为0~1.1 m,最佳爆距范围在0.3~0.45 m之间;根据以上9种工况的分析可知,药量(100、200、300 g)、爆距(0.3、0.6、0.9 m)和冰厚(24、28、32 cm)对破冰半径的影响的主次关系依次为爆距、药量、冰厚。     

水下目标在水下爆炸作用下冲击响应的时频特征

基于某水下目标的抗水下爆炸实验数据,利用小波变换良好的时频局部化性质对监测的水下目标内部装置冲击加速度信号进行时频特征分析,得到了不同频带上冲击信号振动分量的时间历程曲线和能量分布。结果表明,基于冲击信号小波时频特征分析的频带能量可以同时反映冲击振动的强度、频率和持续时间对目标损伤的影响,同时结合不同频带的时间历程曲线可以获得冲击波和二次压力波在不同频带上的分布和衰减的细节信息,由此可确定冲击波和二次压力波各自对目标毁伤的影响。     

冷激波灭火系统中激波对灭火效果和周边环境的影响

为了评估冷激波灭火弹爆炸后形成的激波对灭火效果和周边环境的影响,建立了一套纹影实验装置。通过纹影实验,观察了小尺寸下不同灭火介质爆炸抛撒后激波的形成和传播,并推算了冷激波灭火弹爆炸后油盆边缘附近的波后质点速度。观察发现,水基灭火介质爆炸抛撒后没有形成激波;而粉基灭火介质尽管爆炸抛撒后形成激波,但在油盆边缘附近激波强度较弱,波后质点速度小。与介质抛撒引起的可燃气体介质运动相比,激波对加快可燃气体介质运动的影响可以忽略。最后,通过高速摄影实验验证了激波对灭火效果的影响是可以忽略的。因此,冷激波系统中,激波对灭火效果和周边环境的影响是可以忽略的。     

声振耦合分析在冲击波测量中的应用

为了高精度地测量空气冲击波形,采用声振耦合分析对该测量系统的频响特性进行了理论计算,并在激波管中进行了动态响应实验。通过上述研究,得出了探头在3个不同量程时的适宜阻尼孔径。结果表明,探头的阻尼孔直径和波形上升时间的计算值与实验值都是基本符合的,并且该测量系统在强爆炸中测得的冲击波压力波形也具有良好的频响特性。     

Oblique shock wave with sweep

An attached planar, oblique shock with sweep is investigated for the inviscid flow of a perfect gas. The ratio of specific heats, freestream Mach number, and wedge angle in the plane of the freestream velocity are prescribed, with the sweep angle as a free parameter. Explicit relations are provided for jump and detachment conditions. A number of trends, some non-intuitive, are discussed, e.g., the downstream Mach number may increase with sweep.     

On the nonlinear stability of a swirling liquid jet

The nonlinear deformation and atomization of a rotating column is considered using an axisymmetric boundary element formulation. Swirl has been considered by superposing a potential vortex to the bulk flow of the jet. The resulting model has been shown to reproduce the classical linear result due to Ponstein and parametric studies are conducted in the nonlinear regime to determine wave shapes and droplet sizes. As with prior nonlinear column breakup studies, results indicate that satellite drops are formed from the main wave under virtually all conditions. The ratio of the main drop to satellite drop diameter is shown to be remarkably constant over a variety of wave numbers/column lengths thereby providing a potential approach to produce tightly controlled bimodal sprays.     

基于改进HHT的水中爆炸冲击波信号时频特性分析方法

根据水中爆炸冲击波信号的特征,利用希尔伯特-黄变换(HHT)处理非平稳信号的优势,提出了一种结合小波分解及相关系数筛选的改进HHT方法.该方法首先通过小波分解将信号分为高频部分和低频部分,然后利用相关系数对固有模态函数(IMF)分量进行筛选.理论与实践表明,改进的HHT方法能够有效、准确地对水中爆炸冲击波信号的时频信息...     

Oblique shock wave with sweep II

This article was processed using Springer-Verlag T_EX Shock Waves macro package 1.0 and the AMS fonts, developed by the American Mathematical Society.     

The criterion of the existence or inexistence of transverse shock wave at wedge supported oblique detonation wave

A simplified theoretic method and numerical simulations were carried out to investigate the characterization of propagation of transverse shock wave at wedge supported oblique detonation wave.After solution validation,a criterion which is associated with the ratio Φ (u 2 /u CJ) of existence or inexistence of the transverse shock wave at the region of the primary triple was deduced systematically by 38 cases.It is observed that for abrupt oblique shock wave (OSW)/oblique detonation wave (ODW) transition,a transverse shock wave is generated at the region of the primary triple when Φ < 1,however,such a transverse shock wave does not take place for the smooth OSW/ODW transition when Φ > 1.The parameter Φ can be expressed as the Mach number behind the ODW front for stable CJ detonation.When 0.9 < Φ < 1.0,the reflected shock wave can pass across the contact discontinuity and interact with transverse waves which are originating from the ODW front.When 0.8 < Φ < 0.9,the reflected shock wave can not pass across the contact discontinuity and only reflects at the contact discontinuity.The condition (0.8 < Φ < 0.9) agrees well with the ratio (D ave /D CJ) in the critical detonation.