Integration and validation of some modules for modelling of high-speed chemically reactive flows in two-phase gas-droplet mixtures

被引:1
|
作者
Zhu, Ruixuan [1 ]
Huang, Zhiwei [2 ]
Xu, Chao [3 ]
Wu, Bifen [4 ]
Davy, Martin [1 ]
机构
[1] Univ Oxford, Dept Engn Sci, Oxford OX1 3PJ, England
[2] Shanghai Jiao Tong Univ, Sch Aeronaut & Astronaut, Shanghai 200240, Peoples R China
[3] Argonne Natl Lab, Energy Syst Div, Lemont, IL 60439 USA
[4] ExxonMobil Technol & Engn Co, Spring, TX 77389 USA
基金
上海市自然科学基金;
关键词
Two-phase reacting flow; Multi-component diffusion; Eulerian-Lagrangian solver; Sparse ODE solver; Dynamic adaptive hybrid integration; Detonation wave; NUMERICAL-SIMULATION; CONSERVATION-LAWS; CENTRAL SCHEMES; HEAT-TRANSFER; COMBUSTION; DETONATION; DIFFUSION; SEMIDISCRETE; MECHANISM; SOLVER;
D O I
10.1016/j.compfluid.2024.106282
中图分类号
TP39 [计算机的应用];
学科分类号
081203 ; 0835 ;
摘要
Three modules are integrated into the built-in OpenFOAM rhoCentralFoam solver towards accurate and efficient modelling of high-speed chemically reactive flows in two-phase gas-droplet mixtures within the OpenFOAM 10.0 framework. The first module is the mixture-averaged diffusion model. The second module is the built-in OpenFOAM Lagrangian solver coupled with optimised droplet drag coefficient and convective heat transfer coefficient sub-models. The last module is a sparse stiff chemistry solver based on dynamic adaptive hybrid integration (AHI-S). The optimised droplet sub-models are first verified in correct implementation for subsequent simulations in this work. They show good accuracy against experimental and analytical data in the modelling of ammonia droplet acceleration and cooling in the flowing and/or low-temperature air. The accuracy and efficiency gains related to the mixture-averaged diffusion model and the AHI-S chemistry solver are examined by simulating 1-D detonation propagation in ammonia droplet-free/laden ammoniaoxygen mixtures. Numerical results of detonation propagation speed, gaseous temperature, density, and species distributions around the induction zone show good agreement with experimental data and analytical solutions. Compared to the built-in OpenFOAM diffusion model, the mixture-averaged diffusion model provides different numerical predictions of pulsating instabilities in detonation propagation. It shows better accuracy in depicting the detonation structure within the droplet-free section attributed to improved multi-component diffusion modelling. Compared to the built-in OpenFOAM solver EulerImplicit (backward Euler), the AHI-S chemistry solver reduces the computational cost by around 50%. It achieves satisfactory accuracy in calculating detonation propagation speed within the droplet-free section with the optimal efficiency when the safety factor, beta, equals 0.5.
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页数:17
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共 21 条
  • [1] Generation of two-phase gas-droplet flows with specified characteristics
    Ishmatov A.N.
    Elesin V.V.
    Trubnikov A.A.
    Ogorodnikov S.P.
    [J]. Atmospheric and Oceanic Optics, 2013, 26 (6) : 556 - 558
  • [2] An Evaluation Method for Liquid Separation Structures in Gas-Droplet Two-Phase Flows
    Li, Xing
    Pei, Binbin
    Pei, Huan
    Zhang, Haibin
    Bai, Bofeng
    [J]. HEAT TRANSFER ENGINEERING, 2022, 43 (8-10) : 694 - 707
  • [3] Eulerian-Lagrangian modelling of detonative combustion in two-phase gas-droplet mixtures with OpenFOAM: Validations and verifications
    Huang, Zhiwei
    Zhao, Majie
    Xu, Yong
    Li, Guangze
    Zhang, Huangwei
    [J]. FUEL, 2021, 286
  • [4] Velocity slip and interfacial momentum transfer in the transient section of supersonic gas-droplet two-phase flows
    Wei, WY
    Zhu, JH
    Xia, SL
    Dai, GQ
    Gao, XD
    [J]. CHINESE JOURNAL OF CHEMICAL ENGINEERING, 2002, 10 (02) : 163 - 169
  • [5] Velocity Slip and Interfacial Momentum Transfer in the Transient Section of Supersonic Gas-Droplet Two-Phase Flows
    魏文韫
    朱家骅
    夏素兰
    戴光清
    高旭东
    [J]. Chinese Journal of Chemical Engineering, 2002, (02) : 31 - 37
  • [6] Simulating two-phase flows inside high-speed injectors
    Heister, SD
    [J]. COMPUTATIONAL METHODS IN MULTIPHASE FLOW, 2001, 29 : 253 - 263
  • [7] NUMERICAL MODELING OF TURBULENTEVAPORATING GAS-DROPLET TWO-PHASE FLOWS IN AN AFTERBURNER DIFFUSOR OF TURBO-FAN JET ENGINES
    Zhou Lixing and Zhang JianTsinghua University
    [J]. Chinese Journal of Aeronautics, 1990, (04) : 258 - 265
  • [8] Image processing techniques for high-speed videometry in horizontal two-phase slug flows
    do Amaral, C. E. F.
    Alves, R. F.
    da Silva, M. J.
    Arruda, L. V. R.
    Dorini, L.
    Morales, R. E. M.
    Pipa, D. R.
    [J]. FLOW MEASUREMENT AND INSTRUMENTATION, 2013, 33 : 257 - 264
  • [9] Single- and two-phase fluid droplet breakup in impulsively generated high-speed flow
    Leung, J.
    Gurunadhan, M.
    Menon, S.
    [J]. SHOCK WAVES, 2023, 33 (05) : 385 - 399
  • [10] Single- and two-phase fluid droplet breakup in impulsively generated high-speed flow
    J. Leung
    M. Gurunadhan
    S. Menon
    [J]. Shock Waves, 2023, 33 : 385 - 399