共查询到19条相似文献,搜索用时 140 毫秒
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为了确定空气间隙和金属隔层对冲击起爆的影响,采用火炮加载蓝宝石飞片冲击起爆Φ50 mm×30 mm的A型炸药,产生的冲击波通过空气间隙和金属隔层起爆Φ50 mm的台阶型B型炸药。在B型炸药的后界面粘贴镀膜氟化锂(LiF)窗口,使用光子多普勒测速仪(PDV)测量金属和B型炸药的后界面速度,进而计算得到金属和B型炸药的冲击波透射压力,再利用阻抗匹配计算得到金属和B型炸药的入射压力。结果表明:传爆药和金属隔层间的空气间隙使冲击压缩过程转变为准等熵压缩和冲击压缩两个过程,同时使冲击波的幅值减小;确定了金属隔层厚度为5 mm时冲击波压力的衰减范围;当使用A型炸药作为传爆药,空气间隙为0.3 mm,金属隔层厚度为5 mm时,B型炸药在7~10 mm之间开始反应。 相似文献
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为了系统地研究铝氧比对含铝炸药水下爆炸载荷及能量输出结构的影响,在验证数值模型有效性的基础上,针对铝氧比分别为0、0.16、0.36、0.63的RDX基含铝炸药,利用耦合欧拉-拉格朗日方法模拟了其水下爆炸连续的全过程,考虑了冲击波载荷和气泡载荷之间的耦合作用,从冲击波、气泡和能量输出结构三方面对影响效应进行评估。计算结果表明:随着铝氧比的增大,含铝炸药水下爆炸冲击波衰减时间常数、冲击波冲量、气泡脉动周期、气泡最大半径以及比气泡能都增大;铝氧比为0.36时,冲击波峰值压力、冲击波能流密度和比冲击波能达到最大。铝粉的加入对气泡能的提高相对于冲击波能更加显著。 相似文献
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研究水下爆炸中的防护层问题,将爆炸气体、水、防护层或其他材料看成一个混合流场后,它们的物理状态可以直接用统一形式的Mie-Grüneisen状态方程来表示,再用Mie-Grüneisen混合模型模拟爆炸气体、水、固态防护层之间的复杂相互作用。计算时,通过状态方程中的特定参数来区分流体成分的物理特性,并通过体积分数来区分界面,同时添加自由进出口边界条件;计算过程中,对防护层的效果进行细致研究。研究发现,防护层的效果取决于材料的冲击阻抗。当冲击波从一种介质进入新介质时,在新介质冲击阻抗较小的情况下其压力会降低。同时,进入防护层的冲击波被结构物反射又会形成第二个冲击波。在这个过程中,对防护层的厚度和距离进行关注,但是这两个因素并未产生重要影响。 相似文献
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为研究近场强冲击波对屏蔽装药的冲击引爆效应,通过试验和LS-DYNA3D非线性有限元计算程序对屏蔽压装TNT的冲击引爆进行研究,得到了接触爆炸时压装TNT被引爆的临界屏蔽板厚度和非接触爆炸时屏蔽压装TNT的殉爆距离,分析了非接触爆炸时屏蔽板厚度对殉爆距离的影响,并通过非线性最小二乘法拟合得到屏蔽板厚度与殉爆距离的函数关系。结果表明:数值计算结果与试验结果基本一致;接触爆炸时临界起爆的屏蔽板厚度在20~23 mm之间;屏蔽板采用3 mm厚的45钢时,非接触爆炸作用下压装TNT的殉爆距离在12~15 mm之间;非接触爆炸时殉爆距离随着屏蔽板厚度的增加而减小,当无屏蔽板时,压装TNT的殉爆距离为79 mm,当屏蔽板厚度从1 mm加大到9 mm时,殉爆距离从51 mm减为1.5 mm,被发装药的屏蔽板对冲击波有显著的防护作用。 相似文献
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水下爆炸冲击波作用下空化区域形成的特性研究 总被引:3,自引:0,他引:3
对水下爆炸冲击波作用下的局部空化和区域空化形成特性进行了理论和实验研究.引入平面冲击波假设,理论分析了结构几何尺度及冲击波参数的变化对空化区域形成的影响,并在直径5 m的圆柱形水箱中,对边长1 m、厚度2 mm的方形钢板在50 g TNT炸药、1 m爆距条件下进行了水下爆炸冲击实验,以验证局部空化理论.研究结果表明:在相同的冲击条件下,结构尺度的变化对局部空化的形成具有较大影响;炸药质量及爆深的变化会改变区域空化的形状及范围;实验结果与局部空化理论计算结果基本一致. 相似文献
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Wire Rope Isolators (WRI) are well known and used for the protection of sensitive equipment against non-contact underwater explosions (UNDEX) on board Naval Ships, amongst others, which are extremely destructive and can comple`tely impair the ship’s combat capability.
Traditional WRI exhibit a number of definite advantages, such as large deflection capability, modularity and insensitivity to aggressive environment when proper materials are used. However, their inherent nonlinearity does not always provide the best solution in terms of shock attenuation. (Stiffening tension characteristics)
Fortunately, there are ways to overcome this problem, namely increasing their damping and/ or changing their aspect ratio. It is the purpose of this presentation to show how to overcome this problem and through analysis, by use of validated models of the shock testing machines. The existing technology will be briefly presented and HDWRI (high damping wire rope isolators) vs. conventional WRI responses will be compared on the US Navy shock testing machines of MIL-S-901D.
The US Navy standard MIL-S-901 defines a physical shock testing machine to impact the target before its approval. Different testing machines are used (LWSM, MWSM, FSP, and new DSSM) depending on the weight and size of the target, and on the deck frequency simulated.
The Socitec Group has developed a full model of the various shock testing machines using its in-house developed SYMOS software package. Currently, the Group is in the process of completing a model for the DSSM. 相似文献
Traditional WRI exhibit a number of definite advantages, such as large deflection capability, modularity and insensitivity to aggressive environment when proper materials are used. However, their inherent nonlinearity does not always provide the best solution in terms of shock attenuation. (Stiffening tension characteristics)
Fortunately, there are ways to overcome this problem, namely increasing their damping and/ or changing their aspect ratio. It is the purpose of this presentation to show how to overcome this problem and through analysis, by use of validated models of the shock testing machines. The existing technology will be briefly presented and HDWRI (high damping wire rope isolators) vs. conventional WRI responses will be compared on the US Navy shock testing machines of MIL-S-901D.
The US Navy standard MIL-S-901 defines a physical shock testing machine to impact the target before its approval. Different testing machines are used (LWSM, MWSM, FSP, and new DSSM) depending on the weight and size of the target, and on the deck frequency simulated.
The Socitec Group has developed a full model of the various shock testing machines using its in-house developed SYMOS software package. Currently, the Group is in the process of completing a model for the DSSM. 相似文献
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对带有3 mm左右厚铝壳或钢壳的柱形TNT、RS-211、T/Γ(35/65)以及ROT901装药在水下采用一端点起爆后,水中冲击波超压分布进行了二维数值模拟研究。对该四种炸药的每一种,分别考虑了药量为1 kg、3 kg、5 kg和8 kg四种TNT当量的柱形装药情况。柱形装药的长径比为L/D=1.5左右。计算使用的程序为二维欧拉多流体网格法流体力学计算程序MFIC。给出了水中冲击波超压的空间和时间分布;对铝壳和钢壳两种情况的结果进行了分析、比较;同时给出了缩比模型与1∶1模型之间相应物理量之间的缩比关系。 相似文献
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Fibre-Coupling Zig-Zag Beam Deflection Technology for Investigation of Attenuation Process of Laser-Induced Shock Waves 总被引:1,自引:0,他引:1 下载免费PDF全文
A novel fibre-coupling zig-zag beam deflection technology is developed to investigate the attenuation process of laser-induced shock waves in air. Utilizing ordinal reflections of probe beams by a pair of parallel mirrors, a zig-zag beam field is formed, which has eleven probe beams in the horizontal plane. When a laser-induced shock wave propagates through the testing field, it causes eleven deflection signals one after another. The whole attenuation process of the shock wave in air can be detected and illuminated clearly on one experimental curve. 相似文献
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This study is focused on the propagation behavior and attenuation characteristics of a planar incident shock wave when propagating through an array of perforated plates. Based on a density-based coupled explicit algorithm, combined with a third-order MUSCL scheme and the Roe averaged flux difference splitting method, the Navier–Stokes equations and the realizable k-ε turbulence model equations describing the air flow are numerically solved. The evolution of the dynamic wave and ring vortex systems is effectively captured and analyzed. The influence of incident shock Mach number, perforated-plate porosity, and plate number on the propagation and attenuation of the shock wave was studied by using pressure- and entropy-based attenuation rates. The results indicate that the reflection, diffraction, transmission, and interference behaviors of the leading shock wave and the superimposed effects due to the trailing secondary shock wave are the main reasons that cause the intensity of the leading shock wave to experience a complex process consisting of attenuation, local enhancement, attenuation, enhancement, and attenuation. The reflected shock interactions with transmitted shock induced ring vortices and jets lead to the deformation and local intensification of the shock wave. The formation of nearly steady jets following the array of perforated plates is attributed to the generation of an oscillation chamber for the inside dynamic wave system between two perforated plates. The vorticity diffusion, merging and splitting of vortex cores dissipate the wave energy. Furthermore, the leading transmitted shock wave attenuates more significantly whereas the reflected shock wave from the first plate of the array attenuates less significantly as the shock Mach number increases. The increase in the porosity weakens the suppression effects on the leading shock wave while increases the attenuation rate of the reflected shock wave. The first perforated plate in the array plays a major role in the attenuation of the shock wave. 相似文献
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含气泡水内气泡的空间分布会对线性声传播产生影响,导致实验结论与理论预测存在较大偏差.为解决这一问题,将准晶体近似引入到自洽方法中,导出了考虑空间分布时多分散含气泡水的等效声波波数.考虑到含气泡水内,气泡间存在小范围的聚集趋势(简称丛聚现象),在此基础上引入Neyman-Scott点过程描述了含气泡水内气泡的丛聚现象.分析发现,丛聚时,声速、声衰减的峰值将受到抑制,并向低频偏移,且抑制和频偏现象会随丛聚加剧而变强;随频率远离峰值段,丛聚对声传播的影响逐渐减弱.此外,考虑到空间分布的统计信息提取对相关研究的精确与否起到重要作用,引入了一种比例无偏估计,通过该方法获得了仿真环境下丛聚含气泡水模型的相速度及衰减系数,该建模及统计方法也可为相关实验工作提供理论基础. 相似文献