Chemical-diffusive models for flame acceleration and transition-to-detonation: genetic algorithm and optimisation procedure

被引:37
作者
Kaplan, Carolyn R. [1 ]
Ozgen, Alp [1 ]
Oran, Elaine S. [1 ]
机构
[1] Univ Maryland, Dept Aerosp Engn, College Pk, MD 20742 USA
关键词
chemical-diffusive model; deflagration-to-detonation transition; genetic algorithm; optimisation procedure; NUMERICAL SIMULATIONS; DDT; PROPAGATION; CHANNELS;
D O I
10.1080/13647830.2018.1481228
中图分类号
O414.1 [热力学];
学科分类号
摘要
This paper presents a general approach for developing an automated, fast and flexible procedure to determine the reaction parameters for a simplified chemical-diffusive model to simulate flame acceleration and deflagration-to-detonation transition (DDT) in a stoichiometric methane-air mixture. The procedure uses a combination of a genetic algorithm and Nelder-Mead optimisation scheme to find the optimal reaction parameters for a reaction rate based on an Arrhenius form for conversion of reactants to products. The model finds six optimal reaction parameters that reproduce six flame and detonation properties. Results show that the reaction parameters closely reproduce their intended flame and detonation properties. The laminar flame profile computed using the reaction parameters in a 1D Navier-Stokes code matches the profile obtained when using a detailed chemical reaction mechanism. The optimal reaction parameters are then used in a 2D simulation of flame acceleration and DDT in an obstacle-laden channel containing stoichiometric methane-air, and the results show that the computation closely follows the transition-to-detonation observed in experiments. This automated procedure for finding parameters for a proposed reaction model makes it possible to simulate the behaviour of flames and detonations in large, complex scenarios, which would otherwise be an incalculable problem.
引用
收藏
页码:67 / 86
页数:20
相关论文
共 34 条
  • [1] [Anonymous], 2015, BOXL
  • [2] [Anonymous], 1989, GENETIC ALGORITHMS S
  • [3] [Anonymous], 2016, CANTERA OBJECT ORIEN
  • [4] [Anonymous], GRI-Mech 3(0)
  • [5] On the use of immersed boundary methods for shock/obstacle interactions
    Chaudhuri, Arnab
    Hadjadj, Abdellah
    Chinnayya, Ashwin
    [J]. JOURNAL OF COMPUTATIONAL PHYSICS, 2011, 230 (05) : 1731 - 1748
  • [6] Flame acceleration and transition to detonation in ducts
    Ciccarelli, G.
    Dorofeev, S.
    [J]. PROGRESS IN ENERGY AND COMBUSTION SCIENCE, 2008, 34 (04) : 499 - 550
  • [7] Doering W., 1943, ANN PHYS-NEW YORK, V43, P421, DOI DOI 10.1002/ANDP.19434350605
  • [8] Explosion Dynamics Laboratory California Institute of Technology, 2015, SHOCK DET TOOLB CANT
  • [9] Gamezo V.N., 2009, 440 AIAA
  • [10] Flame acceleration and DDT in channels with obstacles: Effect of obstacle spacing
    Gamezo, Vadim N.
    Ogawa, Takanobu
    Oran, Elaine S.
    [J]. COMBUSTION AND FLAME, 2008, 155 (1-2) : 302 - 315