...
首页> 外文期刊>Shock Waves >Mechanism of deflagration-to-detonation transitions above repeated obstacles
【24h】

Mechanism of deflagration-to-detonation transitions above repeated obstacles

机译:重复障碍物上方爆燃-爆轰过渡的机理

获取原文
获取原文并翻译 | 示例
           

摘要

Experiments are carried out to investigate the mechanism of the deflagration-to-detonation transition (DDT). Because, this mechanism has relevance to safety issues in industries, where combustible premixed gases are in general use. A stoichiometric gas of oxygen and hydrogen (oxy-hydrogen) is ignited in a tube, repeated obstacles are installed, and the DDT behaviours are visualized using a high-speed video camera. The pitch and height of the repeated obstacles and the initial pressure of the oxy-hydrogen premixed gas are varied in an attempt to obtain the optimum conditions that cause DDT a short distance from the ignition source. The experiments identified DDT as being essentially caused by one of the following mechanisms: (1) A deflagration wave is accelerated in terms of a vortex, which is generated behind the obstacle, and the flame acceleration induces a secondary shock wave. Eventually, the shock–flame interaction ahead of the obstacle causes DDT via a very strong local explosion. (2) Each shock wave generated by relatively weak local explosions between the obstacles is not sufficient to cause DDT directly, but DDT results from an accumulation of shock waves. The detonation induction distance is also examined, taking into account the physical and chemical parameters of the obstacles and the oxy-hydrogen premixed gas.
机译:进行实验以研究爆燃-爆轰过渡(DDT)的机理。因为,这种机制与普遍使用可燃预混气体的工业中的安全问题有关。在管中点燃氧气和氢气的化学计量气体(氢氧),安装重复的障碍物,并使用高速摄像机将DDT行为可视化。改变障碍物的间距和高度以及氢氧预混合气体的初始压力,以试图获得使DDT与点火源相距较短距离的最佳条件。实验确定DDT基本上是由以下机制之一引起的:(1)爆燃波根据障碍物后面产生的涡流而加速,并且火焰加速度会引发二次冲击波。最终,障碍物前方的冲击与火焰相互作用会通过非常强烈的局部爆炸而引起DDT。 (2)障碍物之间相对较弱的局部爆炸所产生的每个冲击波都不足以直接导致DDT,但是DDT是由冲击波的积累而产生的。还考虑了障碍物和氢氧预混气体的物理和化学参数,检查了爆炸起爆距离。

著录项

  • 来源
    《Shock Waves》 |2012年第6期|p.627-639|共13页
  • 作者单位

    Graduate School of Science and Engineering, Saitama University, 255 Shimo-Ohkubo, Sakura-ku, Saitama-shi, Saitama, 338-8570, Japan;

    Graduate School of Science and Engineering, Saitama University, 255 Shimo-Ohkubo, Sakura-ku, Saitama-shi, Saitama, 338-8570, Japan;

    Graduate School of Science and Engineering, Saitama University, 255 Shimo-Ohkubo, Sakura-ku, Saitama-shi, Saitama, 338-8570, Japan;

  • 收录信息
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Deflagration-to-detonation transition; Detonation induction distance; Shock wave; Local explosion; Obstacle;

    机译:爆燃-爆轰过渡爆轰感应距离冲击波局部爆炸障碍物;

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号