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  • Zhan, Ningyu  (8)
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  • 1
    Online Resource
    Online Resource
    Wiley ; 2021
    In:  International Journal for Numerical Methods in Fluids Vol. 93, No. 5 ( 2021-05), p. 1378-1395
    In: International Journal for Numerical Methods in Fluids, Wiley, Vol. 93, No. 5 ( 2021-05), p. 1378-1395
    Abstract: In this work, a meshfree Lattice Boltzmann Flux Solver (LBFS) is proposed to resolve compressible flow problems based on scattered points without mesh connections. The new method employs the Least Square‐based Finite Difference (LSFD) scheme to discretize the governing equations. In order to simulate discontinuous problems such as shock wave, the mid‐point between two adjacent nodes is regarded as a discontinuous interface over which the Riemann problem is established. The local fluxes at this interface point are reconstructed by LBFS using the local solution of the Lattice Boltzmann Equation (LBE) as well as its correlations to macroscopic variables and moment relations. The LBFS is constructed based on the non‐free parameter D1Q4 model: the normal component of the particle velocity on the interface is retained, while the tangential component is reconstructed by the macroscopic variables on both sides of the interface. The meshfree LBFS expects some intriguing merits. On one hand, it inherits the physical robustness of the LBFS: the local fluxes are reconstructed from the physical solutions instead of mathematical interpolations. On the other hand, it allows the implementation at arbitrarily distributed nodes, which credits to the flexibility of the method. Representative examples of compressible flows, including Sod shock tube, Osher‐Shu shock tube, flow around NACA0012 airfoil, flow around staggered NACA0012 biplane configuration and shock reflection problem, are simulated by the proposed method for comprehensive evaluation of the meshfree LBFS.
    Type of Medium: Online Resource
    ISSN: 0271-2091 , 1097-0363
    URL: Issue
    Language: English
    Publisher: Wiley
    Publication Date: 2021
    detail.hit.zdb_id: 245720-9
    detail.hit.zdb_id: 1491176-0
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  • 2
    Online Resource
    Online Resource
    MDPI AG ; 2022
    In:  Entropy Vol. 24, No. 11 ( 2022-11-08), p. 1622-
    In: Entropy, MDPI AG, Vol. 24, No. 11 ( 2022-11-08), p. 1622-
    Abstract: A simplified linearized lattice Boltzmann method (SLLBM) suitable for the simulation of acoustic waves propagation in fluids was proposed herein. Through Chapman–Enskog expansion analysis, the linearized lattice Boltzmann equation (LLBE) was first recovered to linearized macroscopic equations. Then, using the fractional-step calculation technique, the solution of these linearized equations was divided into two steps: a predictor step and corrector step. Next, the evolution of the perturbation distribution function was transformed into the evolution of the perturbation equilibrium distribution function using second-order interpolation approximation of the latter at other positions and times to represent the nonequilibrium part of the former; additionally, the calculation formulas of SLLBM were deduced. SLLBM inherits the advantages of the linearized lattice Boltzmann method (LLBM), calculating acoustic disturbance and the mean flow separately so that macroscopic variables of the mean flow do not affect the calculation of acoustic disturbance. At the same time, it has other advantages: the calculation process is simpler, and the cost of computing memory is reduced. In addition, to simulate the acoustic scattering problem caused by the acoustic waves encountering objects, the immersed boundary method (IBM) and SLLBM were further combined so that the method can simulate the influence of complex geometries. Several cases were used to validate the feasibility of SLLBM for simulation of acoustic wave propagation under the mean flow.
    Type of Medium: Online Resource
    ISSN: 1099-4300
    Language: English
    Publisher: MDPI AG
    Publication Date: 2022
    detail.hit.zdb_id: 2014734-X
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  • 3
    Online Resource
    Online Resource
    AIP Publishing ; 2021
    In:  Physics of Fluids Vol. 33, No. 6 ( 2021-06-01)
    In: Physics of Fluids, AIP Publishing, Vol. 33, No. 6 ( 2021-06-01)
    Abstract: In this work, a discrete gas-kinetic scheme (DGKS) based on the arbitrary Lagrangian–Eulerian (ALE) method is proposed for the simulation of moving boundary problems. The governing equations are the ALE-based Navier–Stokes equations, which are discretized using the finite volume method. Starting from a circular function-based Boltzmann equation, a grid motion term is introduced to obtain the Boltzmann equation in ALE form. Based on the moment relations and Chapman–Enskog analysis, the moment of particle velocity and distribution function are summed to obtain the fluxes. The DGKS expression in the ALE framework can then be derived. In this method, the flux at the cell interface can be calculated from the local solution of the Boltzmann equation, which is physically realistic and makes the algorithm more stable. As DGKS is based on a multidimensional particle velocity model, it is not necessary to use approximate values for the reconstruction process. In addition, DGKS can simultaneously handle inviscid and viscous fluxes when simulating viscous flow problems, resulting in a higher degree of consistency. Finally, several moving boundary examples are simulated to validate the ALE-DGKS method. The results show the algorithm was observed to achieve second-order accuracy and can solve moving boundary problems effectively.
    Type of Medium: Online Resource
    ISSN: 1070-6631 , 1089-7666
    Language: English
    Publisher: AIP Publishing
    Publication Date: 2021
    detail.hit.zdb_id: 1472743-2
    detail.hit.zdb_id: 241528-8
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  • 4
    Online Resource
    Online Resource
    Elsevier BV ; 2022
    In:  Computers & Mathematics with Applications Vol. 114 ( 2022-05), p. 21-40
    In: Computers & Mathematics with Applications, Elsevier BV, Vol. 114 ( 2022-05), p. 21-40
    Type of Medium: Online Resource
    ISSN: 0898-1221
    RVK:
    Language: English
    Publisher: Elsevier BV
    Publication Date: 2022
    detail.hit.zdb_id: 2004251-6
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  • 5
    Online Resource
    Online Resource
    Elsevier BV ; 2023
    In:  Journal of Computational Physics Vol. 490 ( 2023-10), p. 112300-
    In: Journal of Computational Physics, Elsevier BV, Vol. 490 ( 2023-10), p. 112300-
    Type of Medium: Online Resource
    ISSN: 0021-9991
    Language: English
    Publisher: Elsevier BV
    Publication Date: 2023
    detail.hit.zdb_id: 160508-2
    detail.hit.zdb_id: 1469164-4
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  • 6
    In: Computers & Mathematics with Applications, Elsevier BV, Vol. 156 ( 2024-02), p. 103-120
    Type of Medium: Online Resource
    ISSN: 0898-1221
    RVK:
    Language: English
    Publisher: Elsevier BV
    Publication Date: 2024
    detail.hit.zdb_id: 2004251-6
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  • 7
    Online Resource
    Online Resource
    AIP Publishing ; 2021
    In:  Physics of Fluids Vol. 33, No. 1 ( 2021-01-01)
    In: Physics of Fluids, AIP Publishing, Vol. 33, No. 1 ( 2021-01-01)
    Abstract: A meshfree method based on the discrete gas-kinetic scheme (DGKS) (called the meshfree-DGKS) for simulation of incompressible/compressible flows is proposed in this work. In this approach, the governing equations are discretized using the meshfree method based on the least squares-based finite difference approach. To simulate compressible problems with discontinuities, the virtual mid-points between adjacent nodes, which are regarded as Riemann discontinuities, are established. Then, the concept of numerical flux is introduced, which enables computing both compressible and incompressible problems. The fluxes at the mid-points are calculated using the DGKS based on the discrete particle velocity model. The corresponding particle velocity components and distribution functions are integrated based on moment relations to obtain the flux. The meshfree-DGKS maintains the advantages of the meshless method as it is implemented at arbitrarily distributed nodes. This breaks through the limitations of the grid topology and is suitable to handle complex geometries. More importantly, the fluxes at the mid-point are reconstructed with the DGKS using the local solution of the Boltzmann equation, which can describe its physical properties well, thus easily and stably capturing the shock wave. In addition, the DGKS can simultaneously calculate inviscid and viscous fluxes when simulating viscous flow problems, which gives an improved algorithm consistency. Several representative examples, such as shock tube problems, implosion problem, couette flow, lid-driven cavity flow, flow in a channel with a backward-facing step, supersonic flow around a ramp segment, and flow around staggered NACA0012 biplane configuration, are simulated to validate the proposed meshfree-DGKS.
    Type of Medium: Online Resource
    ISSN: 1070-6631 , 1089-7666
    Language: English
    Publisher: AIP Publishing
    Publication Date: 2021
    detail.hit.zdb_id: 1472743-2
    detail.hit.zdb_id: 241528-8
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  • 8
    Online Resource
    Online Resource
    American Physical Society (APS) ; 2022
    In:  Physical Review E Vol. 105, No. 6 ( 2022-6-21)
    In: Physical Review E, American Physical Society (APS), Vol. 105, No. 6 ( 2022-6-21)
    Type of Medium: Online Resource
    ISSN: 2470-0045 , 2470-0053
    RVK:
    Language: English
    Publisher: American Physical Society (APS)
    Publication Date: 2022
    detail.hit.zdb_id: 2844562-4
    SSG: 12
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