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LUO Shuangshuang, YANG Yiren, SUN Jianwei, CHEN Hao. Adaptive Mesh Refinement and Continuum Surface Force Method for Complex Two-Phase Flows[J]. Journal of Southwest Jiaotong University. doi: 10.3969/j.issn.0258-2724.20240263
Citation: LUO Shuangshuang, YANG Yiren, SUN Jianwei, CHEN Hao. Adaptive Mesh Refinement and Continuum Surface Force Method for Complex Two-Phase Flows[J]. Journal of Southwest Jiaotong University. doi: 10.3969/j.issn.0258-2724.20240263

Adaptive Mesh Refinement and Continuum Surface Force Method for Complex Two-Phase Flows

doi: 10.3969/j.issn.0258-2724.20240263
  • Received Date: 31 May 2024
  • Rev Recd Date: 08 Jan 2025
  • Available Online: 25 Mar 2026
  • To address two-phase flow problems with complex gas-liquid interface topology variation, a numerical simulation method capable of balancing computational efficiency and interface resolution accuracy was proposed. First, quadtree/octree Cartesian meshes with tree data structures were employed for spatial discretization. Adaptive mesh refinement was developed by leveraging the mesh’s hierarchical structures. Second, the continuum surface force (CSF) model was implemented within the adaptive mesh framework. By applying double convolution blurring to the volume fraction, the surface tension was smoothly distributed to the interface neighborhood, and the piecewise linear interface reconstruction technique was utilized to track the gas-liquid interface accurately. Subsequently, a mesh refinement criterion was established, and both the discrete error based on wavelet analysis of flow field velocity and the interface curvature distribution were considered, thereby achieving dynamic refinement in regions with sharp flow field variations and phase boundaries. Finally, the accuracy and reliability of the algorithm were validated through numerical examples of classic gas-liquid two-phase flow. The results show that in the verification of the Laplace law of surface tension, when the interface curvature is adopted as the refinement criterion, the computational error of internal and external pressure difference is only about 3.0%, which is significantly superior to the error range from 7.5% to 24% when using the volume fraction as the criterion, and its accuracy is consistent with that of uniform fine meshes. The proposed method can reduce the computational time consumption by approximately one order of magnitude compared with uniform fine meshes. In the numerical examples of surface tension waves, the root mean square error between the numerical solution and the theoretical solutions of regular modal can be reduced to the order of 10−5. In the simulation of a head-on collision between binary droplets, the experimentally observed dumbbell-shaped and diamond-shaped deformation sequences are reproduced, and the complex interface topology evolution details such as gas film rupture and the formation of tiny bubbles are captured.

     

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