Numerical modeling of plasma assisted deflagration to detonation transition in a microscale channel

被引:0
|
作者
Shi, Zhiyu [1 ]
Mao, Xingqian [1 ]
Thawko, Andy [1 ]
Ju, Yiguang [1 ,2 ]
机构
[1] Princeton Univ, Dept Mech & Aerosp Engn, Princeton, NJ 08544 USA
[2] Princeton Plasma Phys Lab, Princeton, NJ 08540 USA
关键词
Non-equilibrium plasma; Deflagration to detonation transition; Zel'dovich gradient mechanism; Autoignition; Ignition-shock wave coupling; HYBRID REPETITIVE NANOSECOND; FLAME ACCELERATION; IGNITION; COMBUSTION; MULTITIMESCALE; ENHANCEMENT;
D O I
10.1016/j.proci.2024.105659
中图分类号
O414.1 [热力学];
学科分类号
摘要
This work numerically studies the plasma assisted deflagration to detonation transition (DDT) of H2/O2 2 /O 2 mixtures in a microscale channel with detailed chemistry and transport. The results show that the DDT onset time is non- monotonically dependent on the discharge pulse number. The DDT is accelerated with small pulse numbers, whereas retarded with large ones. Two different DDT regimes, respectively at a small and large plasma discharge number, via acoustic choking of the burned gas and plasma-enhanced reactivity gradient without acoustic choking, are observed. Without plasma discharge, pronounced pressure and temperature gradients in front of the flame are generated by acoustic compression after the choking of the burned gas, triggering DDT via auto- ignition. With small plasma pulse numbers, the plasma-generated species enhance the ignition kinetics and lead to an increased reactivity in the boundary layer. After the choking of the burned gas, the plasma-enhanced reactivity advances the sequence of autoignition near the wall, strengthens ignition-shock wave coupling, and accelerates DDT. However, with a large discharge pulse number, a direct autoignition initiating DDT can occur without the acoustic choking of the burned gas due to the strongly accelerated reactivity and elevated temperature. In this case, DDT onset is retarded because the elevated temperature increases sonic velocity and the increased reactivity accelerates fuel oxidation in front of the flame, decelerating the formation of a leading shock and subsequent pressure buildup ahead of the flame. The present modeling reveals that no matter with or without plasma discharge, DDT is initiated by autoignition in thermal, pressure, and reactivity gradient fields via the Zel'dovich gradient mechanism. The acoustic choking of the burned gas may not be the necessary condition of DDT with strong plasma-enhanced reactivity gradient. This work provides an answer to the experimentally observed non-monotonic DDT onset time by plasma, which provides guidance to control DDT in advanced detonation engines and fire safety of hydrogen-fueled catalytic reactors in microchannels by non-equilibrium plasma discharge.
引用
收藏
页数:8
相关论文
共 50 条
  • [1] Plasma-assisted ignition and deflagration-to-detonation transition
    Starikovskiy, Andrey
    Aleksandrov, Nickolay
    Rakitin, Aleksandr
    PHILOSOPHICAL TRANSACTIONS OF THE ROYAL SOCIETY A-MATHEMATICAL PHYSICAL AND ENGINEERING SCIENCES, 2012, 370 (1960): : 740 - 773
  • [2] NUMERICAL MODELING OF DEFLAGRATION-TO-DETONATION TRANSITION IN POROUS EXPLOSIVES
    KIM, K
    BULLETIN OF THE AMERICAN PHYSICAL SOCIETY, 1979, 24 (04): : 722 - 722
  • [3] Numerical simulation of the deflagration to detonation transition
    M. T. Parra-Santos
    F. Castro-Ruiz
    C. Méndez-Bueno
    Combustion, Explosion and Shock Waves, 2005, 41 : 215 - 222
  • [4] Numerical simulation of the deflagration to detonation transition
    Parrra-Santos, MT
    Castro-Ruiz, F
    Méndez-Bueno, C
    COMBUSTION EXPLOSION AND SHOCK WAVES, 2005, 41 (02) : 215 - 222
  • [5] Effect of Plasma on the Deflagration to Detonation Transition
    Tropina, Albina A.
    Mahamud, Rajib
    COMBUSTION SCIENCE AND TECHNOLOGY, 2022, 194 (13) : 2752 - 2770
  • [6] Numerical modeling of deflagration to detonation transition in inhomogeneous hydrogen/air mixtures
    Azadboni, Reza Khodadadi
    Wen, Jennifer X.
    Heidari, Ali
    Wang, Changjian
    JOURNAL OF LOSS PREVENTION IN THE PROCESS INDUSTRIES, 2017, 49 : 722 - 730
  • [7] Numerical Modeling of Flame Acceleration and Transition from Deflagration to Detonation Using OpenFOAM®
    Azadboni, Reza Khodadadi
    Wen, Jennifer X.
    Heidari, Ali
    OPENFOAM(R), 2019, : 357 - 372
  • [8] Numerical Analysis of the Deflagration to Detonation Transition in Primary Explosives
    Trzcinski, Waldemar A.
    CENTRAL EUROPEAN JOURNAL OF ENERGETIC MATERIALS, 2012, 9 (01): : 17 - 38
  • [9] A numerical study of the rapid deflagration-to-detonation transition
    Wang, Yuqi
    Liang, Jianhan
    Deiterding, Ralf
    Cai, Xiaodong
    Zhang, Lin
    PHYSICS OF FLUIDS, 2022, 34 (11)
  • [10] ON NUMERICAL MODELING OF TRANSITION FROM DEFLAGRATION TO DETONATION IN HOMOGENEOUS COMBUSTIBLE GAS-MIXTURE
    SMIRNOV, NN
    PANFILOV, II
    VESTNIK MOSKOVSKOGO UNIVERSITETA SERIYA 1 MATEMATIKA MEKHANIKA, 1993, (03): : 30 - 41