2019
DOI: 10.1016/j.ast.2019.01.010
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Velocity behavior downstream of perforated plates with large blockage ratio for unstable and stable detonations

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Cited by 50 publications
(8 citation statements)
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“…Wang et al [38] 2017 2.5 32 78.1 15. Zhang et al [34,[39][40][41][42][43][44][45][46][47][48][49][50] 2015-2019 2.5 CT:4/14/36, AC:2/4.5/7 1250 galloping detonations, spinning detonations, and stuttering detonations. Detonation limit conditions are reached through reducing the initial pressure of the combustible mixture, changing the confinement geometry and/or scale, increasing the amount of an inert diluent, changing the roughness of the confinement boundary, etc.…”
Section: Table 1 Previous Literature Of Detonation Propagation Limitsmentioning
confidence: 99%
“…Wang et al [38] 2017 2.5 32 78.1 15. Zhang et al [34,[39][40][41][42][43][44][45][46][47][48][49][50] 2015-2019 2.5 CT:4/14/36, AC:2/4.5/7 1250 galloping detonations, spinning detonations, and stuttering detonations. Detonation limit conditions are reached through reducing the initial pressure of the combustible mixture, changing the confinement geometry and/or scale, increasing the amount of an inert diluent, changing the roughness of the confinement boundary, etc.…”
Section: Table 1 Previous Literature Of Detonation Propagation Limitsmentioning
confidence: 99%
“…This process is often referred to as deflagration‐to‐detonation transition (DDT) 12. Obstacles in the way of the flame propagation have been employed to investigate the transition from deflagration to detonation 13. Significant advances have been made over the years in the understanding of the flame acceleration and DDT processes, which have been outlined in several excellent papers 14–18.…”
Section: Introductionmentioning
confidence: 99%
“…Pang et al [6] conducted explosive experiments in tunnels with various turning angles and obtained the distribution law of a high-temperature flow field before and after the turning. Zhang et al [7] studied the difference in the propagation velocity behavior of the detonation wave after large-scale diffraction and revealed the interaction mechanism between the diffraction wave and the detonation wave. Cheng et al [8] proposed using a nonreactive gas jet (CO 2 ) to promote the formation of the precursor shock wave and the propagation speed of the flame in the deflagration wave and studied the effects of jet pressure and its position and jet parameters on the deflagration propagation.…”
Section: Introductionmentioning
confidence: 99%