Huang Chao-Yuan, Liu Fei, Xin Kai, Gao Yong-Hong, Duan Ya-Peng
Institute of Defense Engineering, AMS, PLA, Luoyang, 471023, China.
Institute of Defense Engineering, AMS, PLA, Beijing, 100850, China.
Sci Rep. 2024 Jun 28;14(1):14897. doi: 10.1038/s41598-024-65797-5.
In order to improve the driving ability of the explosion wave simulation equipment, reduce the erosion effect of condensed explosives on the explosion wave simulation equipment, improve the safety of the test process, and make better use of the meteorological detonation driving method, it is necessary to optimize the source of the shock wave load in the driving section. Based on the finite volume method of FLACS, a methane detonation driving model corresponding to the test is established to explore the feasibility of using methane as an explosion source to test the structure against explosion shock wave. A methane detonation drive test was carried out to verify the accuracy of the numerical model. Finally, an engineering model for attenuation of shock wave overpressure peak value in pipeline is established by dimensional analysis, and the model coefficient is determined by numerical simulation and test data. The results show that the blast pressure is the highest when the methane volume ratio reaches 9.5 vol% in the methane-air mixture. Simply increasing oxygen content has little effect on the peak overpressure and positive pressure duration of shock wave. In the pure oxygen environment, the detonation effect can be achieved when the volume ratio of methane to oxygen is 1:2, and the incident pressure of the shock wave is proportional to the volume of the gas cloud. When the gas cloud volume is constant, a reasonable selection of methane-oxygen mixture ratio can achieve a better detonation effect, which can effectively increase the peak overpressure of the shock wave in the test section. The research results can provide technical reference for the development of new explosion wave simulation equipment.
为提高爆炸波模拟设备的驱动能力,降低凝聚炸药对爆炸波模拟设备的侵蚀作用,提高试验过程的安全性,更好地利用气象爆轰驱动方法,有必要对驱动段冲击波载荷源进行优化。基于FLACS的有限体积法,建立了与试验对应的甲烷爆轰驱动模型,探讨以甲烷作为爆炸源对结构进行抗爆冲击波试验的可行性。开展了甲烷爆轰驱动试验,验证数值模型的准确性。最后,通过量纲分析建立了管道冲击波超压峰值衰减的工程模型,并根据数值模拟和试验数据确定了模型系数。结果表明,甲烷-空气混合物中甲烷体积比达到9.5 vol%时爆炸压力最高。单纯增加氧气含量对冲击波超压峰值和正压作用时间影响不大。在纯氧环境中,甲烷与氧气的体积比为1:2时可实现爆轰效果,且冲击波入射压力与气云体积成正比。当气云体积一定时,合理选择甲烷-氧气混合比可获得较好的爆轰效果,能有效提高试验段冲击波超压峰值。研究结果可为新型爆炸波模拟设备的研制提供技术参考。