Investigations of vortex dynamics driven primary breakup in diesel spray based on multiphase lattice Boltzmann flux solver

被引:0
|
作者
Wang, Yue [1 ]
Li, De-Ming [2 ]
Liu, Jun-Long [2 ]
Zhao, Fei-Yang [1 ]
Yang, Li-Ming [3 ]
Yu, Wen-Bin [1 ]
机构
[1] Shandong Univ, Sch Energy & Power Engn, Jinan 250100, Peoples R China
[2] Weichai Power Co Ltd, State Key Lab Engine & Powertrain Syst, Weifang 261001, Peoples R China
[3] Nanjing Univ Aeronaut & Astronaut, Sch Aerosp Engn, Nanjing 210016, Peoples R China
关键词
INCOMPRESSIBLE 2-PHASE FLOWS; ATOMIZATION; ENGINE;
D O I
10.1063/5.0219056
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
During the fuel injection process, there is competition, merging, and entrainment between the Rayleigh-Taylor and Kelvin-Helmholtz instabilities, eventually leading to the formation of jet turbulence. The associated vortex dynamics is crucial for understanding the micro-evolution of surface waves on fuel spray. Considering the characteristics of fuel jet with large density ratios, a pressure-corrected multiphase lattice Boltzmann flux solver is proposed in this study, coupled with the Cahn-Hilliard model, to capture the micro-scale evolution of diesel spray. The spray evolution during the primary breakup, under simulated engine operating conditions, is systematically conducted by defining the parameters of vortex dynamics. According to the growth feature of vortex velocity, the microscopic evolution during the primary breakup can be divided into five stages: diffusion growth, exponential growth, potential flow growth, re-acceleration, and chaotic mixing (CM), providing a theoretical basis for the instability analysis of spray breakup. The growth of the Rayleigh-Taylor instability is determined by the competitive relationship between buoyancy and viscous dissipation forces. In cases of higher density ratios, the buoyancy-driven Kelvin-Helmholtz and the secondary growth Rayleigh-Taylor waves mutually advance, elongate, disintegrate, and finally breakup. Therefore, the influence of the density ratio on tail velocities shows a scenario of first promoting and then inhibiting. As the density ratio increases, the instability reaches the CM stage of asymmetric development more quickly by undergoing complex vortical motions. At this stage, there is a complicated phenomenology associated with the evolution of spray interface, including multiscale curling, severe deformation, vortex disintegration, and droplet breakup, eventually leading to turbulence.
引用
收藏
页数:13
相关论文
共 50 条
  • [41] An implicit lattice Boltzmann flux solver with a projection-based interpolation scheme for the convection-diffusion equation
    Hong, Peng
    Dai, Chuanshan
    Wang, Guiling
    Lei, Haiyan
    COMPUTERS & MATHEMATICS WITH APPLICATIONS, 2024, 159 : 287 - 301
  • [42] On the investigation of shock wave/boundary layer interaction with a high-order scheme based on lattice Boltzmann flux solver
    Jian Qin
    Haichuan Yu
    Jie Wu
    Advances in Aerodynamics, 2024, 6 (01) : 112 - 132
  • [43] An h-adaptive implicit immersed boundary-lattice Boltzmann flux solver based on JASMIN AMR package
    Zhang, Pan
    Xia, Zhenhua
    Cai, Qingdong
    COMPUTERS & FLUIDS, 2018, 161 : 14 - 22
  • [44] An Implicit Block LU-SGS Algorithm-Based Lattice Boltzmann Flux Solver for Simulation of Hypersonic Flows
    Meng, Z. X.
    Li, S. Z.
    Peng, K.
    Zhang, W. H.
    ADVANCES IN APPLIED MATHEMATICS AND MECHANICS, 2019, 11 (01) : 72 - 90
  • [45] Investigation on the natural convection in horizontal concentric annulus using the variable property-based lattice Boltzmann flux solver
    Cao, Yuhui
    Zhang, Yu
    INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 2017, 111 : 1260 - 1271
  • [46] On the investigation of shock wave/boundary layer interaction with a high-order scheme based on lattice Boltzmann flux solver
    Qin, Jian
    Yu, Haichuan
    Wu, Jie
    ADVANCES IN AERODYNAMICS, 2024, 6 (01)
  • [47] On the investigation of shock wave/boundary layer interaction with a high-order scheme based on lattice Boltzmann flux solver
    Jian Qin
    Haichuan Yu
    Jie Wu
    Advances in Aerodynamics, 6
  • [48] Numerical Investigation on the Deformation of the Free Interface During Water Entry and Exit of a Circular Cylinder by Using the Immersed Boundary-Multiphase Lattice Boltzmann Flux Solver
    Zhang, Guiyong
    Yan, Haoran
    Song, Hong
    Wang, Heng
    Hui, Da
    JOURNAL OF MARINE SCIENCE AND APPLICATION, 2022, 21 (03) : 99 - 113
  • [49] Numerical Investigation on the Deformation of the Free Interface During Water Entry and Exit of a Circular Cylinder by Using the Immersed Boundary-Multiphase Lattice Boltzmann Flux Solver
    Guiyong Zhang
    Haoran Yan
    Hong Song
    Heng Wang
    Da Hui
    Journal of Marine Science and Application, 2022, 21 : 99 - 113
  • [50] Fluid-structure interaction simulation based on immersed boundary-lattice Boltzmann flux solver and absolute nodal coordinate formula
    Liu, Fan
    Liu, Gang
    Shu, Chang
    PHYSICS OF FLUIDS, 2020, 32 (04)