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Self-ignition and explosion of a 13-MPa pressurized unsteady hydrogen jet under atmospheric conditions

机译:大气条件下13 MPa加压不稳定氢射流的自燃和爆炸

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The process of unsteady high-pressure hydrogen release observed on local vessel rupture is investigated experimentally. The flow structure during the formation of a supersonic free hydrogen jet is studied. The obtained data correlates well with the numerical simulation of sonic underexpanded hydrogen jet released into the atmosphere. In particular, it has been confirmed that the Mach disk fluctuates in the case of unsteady outflow of underexpanded hydrogen jet. It has been shown that in order to provide diffusion self-ignition, it is necessary to focus an air shock wave, formed after the vessel rupture, within the studied initial hydrogen tank pressure range. Lab and ground tests on self-ignition and explosion of hydrogen that outflows through a 15-mm opening when the flow interacts with a 37-mm-radius hemispherical cavity are described. A comparison of the diffusion combustion dynamics of releasing hydrogen in self-ignition and induced ignition scenarios is made. The observed visible flame front velocities of 150-220 m/s can result in dangerous blast waves in the case of large-scale hydrogen release. Measures to reduce the risk of explosion of unsteady high-pressure hydrogen jets releasing into an encumbered space are proposed. Copyright (C) 2015, Hydrogen Energy Publications, LLC. Published by Elsevier Ltd. All rights reserved.
机译:实验研究了局部容器破裂时观察到的不稳定氢释放过程。研究了超音速自由氢射流形成过程中的流动结构。所得数据与声速膨胀不足的氢射流释放到大气中的数值模拟具有很好的相关性。特别地,已经证实,在膨胀不足的氢气射流不稳定流出的情况下,马赫盘会发生波动。已经表明,为了提供扩散自燃,有必要将在容器破裂后形成的空气冲击波聚焦在研究的初始氢罐压力范围内。描述了当流体与半径为37 mm的半球形空腔相互作用时从15 mm开口流出的氢的自燃和爆炸的实验室和地面测试。进行了自燃和诱导点火过程中释放氢扩散燃烧动力学的比较。在大规模释放氢气的情况下,观察到的可见火焰前沿速度为150-220 m / s会导致危险的爆炸波。提出了减少不稳定的高压氢射流释放到障碍空间的爆炸危险的措施。 Hydrogen Energy Publications,LLC版权所有(C)2015。由Elsevier Ltd.出版。保留所有权利。

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