冲击波模拟器中爆破压力对空气爆炸发展影响的实验研究

Parker Zieg, J. Benson, Yang Liu
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引用次数: 0

摘要

由于在军事冲突中广泛使用爆炸装置,爆炸性爆炸造成的危及生命的伤害和死亡人数急剧增加。为了更好地了解爆炸波并减轻爆炸波造成的损害,已经开发了各种设备/系统来在实验室条件下复制现场爆炸场景。东卡罗莱纳大学先进的冲击波模拟器(即ECU-ABWS)就是这样一个设施,可以重现各种形状和剖面的冲击波。爆破峰值超压是造成最大损伤的关键因素,其本质上是由爆破压力决定的。因此,迫切需要更好地了解爆炸压力对爆炸产生和发展的影响,以开发更安全、更有效的爆炸缓解技术。本研究在ECU-ABWS中进行了一系列实验,对不同爆炸压力条件下产生的冲击波进行了表征。在使用时间分辨多点压力传感系统测量沿爆炸传播方向多个位置的入射(侧面)压力的同时,还使用高速纹影成像系统定性地揭示了爆炸波剖面的时间演变。压力传感和纹影图像采集的同步使我们能够通过将入射压力和冲击波形态相关联,提取不同爆炸压力条件下动态冲击波发展的更多物理细节。在本研究中,通过改变分离加压气体驱动部分和常压空气驱动部分的膜的厚度来实现不同的破裂压力。结果表明,爆破压力与峰值超压之间存在线性关系。随着破裂压力的增加(通过增加膜厚度),随着峰值超压的增加,也可以观察到更清晰定义的激波阵面。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
An Experimental Study on the Effects of Burst Pressure on Air Blast Development in a Blast Wave Simulator
Due to the extensive use of explosive devices in military conflicts, there has been a dramatic increase in life-threatening injuries and resultant death toll caused by explosive blasts. In an attempt to better understand the blast waves and mitigate the damages caused by such blast waves, various devices/systems have been developed to replicate the field blast scenarios in laboratory conditions. The East Carolina University Advanced Blast Wave Simulator (i.e., ECU-ABWS) is one such facility that can reproduce blast waves of various shapes and profiles. The peak overpressure of a blast is the key factor that causes the greatest number of damages, and it is essentially determined by the burst pressure of the blast. Therefore, a better understanding of the effects of burst pressure on blast generation and development is strongly desired to develop safer and more effective blast mitigation technologies. In the present study, a series of experiments were carried out in the ECU-ABWS to characterize the blast waves generated under different burst pressure conditions. While the incident (side-on) pressures at multiple locations along the blast propagation direction were measured using a temporally-resolved multi-point pressure sensing system, the time-evolutions of blast wave profiles were also qualitatively revealed by using a high-speed Schlieren imaging system. The synchronization of pressure sensing and Schlieren image acquisition enables us to extract more physical details of the dynamic blast wave development under different burst pressure conditions by associating the incident pressures and shock wave morphologies. In this study, the different burst pressures were achieved by altering the thickness of the membrane separating the driver section of pressurized gas and the driven section of air at atmospheric pressure. It is found that there is a linear relationship between the burst pressure and the peak overpressure. As the burst pressure increases (by increasing the membrane thickness), more clearly defined shock wavefronts are also observed along with the peak overpressure increase.
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