Enhanced DDT mechanism from shock-flame interactions in thin channels

被引:15
作者
Yang, Hongxia [1 ,2 ]
Radulescu, Matei, I [2 ]
机构
[1] Northeastern Univ, Fire & Explos Protect Lab, Shenyang 110004, Peoples R China
[2] Univ Ottawa, Dept Mech Engn, Ottawa, ON K1N 6N5, Canada
基金
加拿大自然科学与工程研究理事会;
关键词
Shock-flame interaction; Lambda-shock bifurcation; Deflagration-to-detonation transition; Narrow channel; DETONATION TRANSITION; ACCELERATION; MODEL;
D O I
10.1016/j.proci.2020.07.140
中图分类号
O414.1 [热力学];
学科分类号
摘要
We show experimentally and numerically that when a weak shock interacts with a finger flame in a narrow channel, an extremely efficient mechanism for deflagration to detonation transition occurs. This is demonstrated in a 19-mm-thick channel in hydrogen-air mixtures at pressures below 0.2 atm and weak shocks of Mach numbers 1.5 to 2. The mechanism relies primarily on the straining of the flame shape into an elongated alligator flame maintained by the anchoring mechanism of Gamezo in a bifurcated lambda shock due to boundary layers. The mechanism can increase the flame surface area by more than two orders of magnitude without any turbulence on the flame time scale. The resulting alligator-shaped flame is shown to saturate near the Chapman-Jouguet condition and further slowly accelerate until its burning velocity reaches the sound speed in the shocked unburned gas. At this state, the lead shock and further adiabatic compression of the gas in the induction zone gives rise to auto-ignition and very rapid transition to detonation through merging of numerous spontaneous flames from ignition spots. The entire acceleration can occur on a time scale comparable to the laminar flame time. (c) 2020 The Combustion Institute. Published by Elsevier Inc. All rights reserved.
引用
收藏
页码:3481 / 3495
页数:15
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