4.7 Article

Effects of double-jet positions on detonation initiation characteristics

期刊

AEROSPACE SCIENCE AND TECHNOLOGY
卷 97, 期 -, 页码 -

出版社

ELSEVIER FRANCE-EDITIONS SCIENTIFIQUES MEDICALES ELSEVIER
DOI: 10.1016/j.ast.2019.105609

关键词

Pulse detonation engine; Jet initiation; Double-jet; Jet positions; Detonation initiation; Chemical reaction mechanism

资金

  1. National Natural Science Foundation of China [91741116, 51306153, 91441201]
  2. Natural Science Foundation of Shaanxi Province of China [2017JZ011, 2019JQ-462]
  3. Science and Technology Foundation for Selected Overseas Scholar of Shaanxi Province of China [2017009]
  4. Fundamental Research Funds for the Central Universities [3102017jg02009]

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In order to initiate the detonation waves efficiently, the ignition method of two jets was proposed and utilized to initiate the mixture of H-2/Air in a detonation chamber. The numerical simulation based on H-2/Air detailed chemical reaction kinetics mechanism was carried out to study the influence of the two jets arrangement positions on detonation initiation. The reliability of the numerical simulation was verified by the calculation results of CEA and the experimental results. The simulation results indicated that the distance from the first jet to left end of the detonation chamber (L1) and the distance between the two jets (L2) showed significant influence on the detonation initiation process and the distribution of the reflected shock wave. The reflected wave formed by the reflection between the detonation waves from the jet tubes and the wall contributed to the propagation of the flame and the generation of the plane detonation waves. The OH concentration curve and the temperature curve were coupled. The formation and the consumption of OH was one of the main factors which controlling the detonation waves and the temperature behind the detonation waves. When L1 was greater than 10 mm, the velocity of the detonation waves decreased as L1 increased. Furthermore, when L1 and L2 both equaled to 10 mm, the velocity of the detonation wave was maximized. (C) 2019 Elsevier Masson SAS. All rights reserved.

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