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      다국어 초록 (Multilingual Abstract)

      Immersed boundary method (IBM) is the most effective method to overcome the disadvantage of LBM (Lattice Boltzmann Method) related to the limitation of the grid shape. IBM also make LBM possible to simulate flow over complex shape of obstacle without any treatment on the curved boundary. In the research, IBLBM was used to perform LBM simulation of a flow over a moving circular cylinder to determine the flow feature and aerodynamics characteristic of the cylinder. To ascertain the applicability of IBLBM on the moving obstacle near the wall, it was first simulated for the case of the flow over a fixed circular cylinder in a channel and the results were compared against the solution of moving cylinder in the channel using IBLBM. The simulations were performed in a moderate range of Reynolds number at each moving cylinder to identify the flow feature and aerodynamic characteristics of circular cylinder in a channel. The drag and lift coefficients of the cylinder were calculated from the simulation results. We have numerically confirmed that the critical Reynolds number for vortex shedding is Re=50 and the result is the same as the case of fixed cylinder. As the cylinder approaching to a wall (γ < 2.5), the 2nd vortex is developed by interacting with the wall boundary-layer vorticity. When the cylinder is very closed to the wall, γ < 0.6, the cylinder acts like blockage to block the flow between the cylinder and wall so that the vortex developed on the upper cylinder elongated and time averaged lifting and drag coefficients abruptly increase.
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      Immersed boundary method (IBM) is the most effective method to overcome the disadvantage of LBM (Lattice Boltzmann Method) related to the limitation of the grid shape. IBM also make LBM possible to simulate flow over complex shape of obstacle without ...

      Immersed boundary method (IBM) is the most effective method to overcome the disadvantage of LBM (Lattice Boltzmann Method) related to the limitation of the grid shape. IBM also make LBM possible to simulate flow over complex shape of obstacle without any treatment on the curved boundary. In the research, IBLBM was used to perform LBM simulation of a flow over a moving circular cylinder to determine the flow feature and aerodynamics characteristic of the cylinder. To ascertain the applicability of IBLBM on the moving obstacle near the wall, it was first simulated for the case of the flow over a fixed circular cylinder in a channel and the results were compared against the solution of moving cylinder in the channel using IBLBM. The simulations were performed in a moderate range of Reynolds number at each moving cylinder to identify the flow feature and aerodynamic characteristics of circular cylinder in a channel. The drag and lift coefficients of the cylinder were calculated from the simulation results. We have numerically confirmed that the critical Reynolds number for vortex shedding is Re=50 and the result is the same as the case of fixed cylinder. As the cylinder approaching to a wall (γ < 2.5), the 2nd vortex is developed by interacting with the wall boundary-layer vorticity. When the cylinder is very closed to the wall, γ < 0.6, the cylinder acts like blockage to block the flow between the cylinder and wall so that the vortex developed on the upper cylinder elongated and time averaged lifting and drag coefficients abruptly increase.

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      목차 (Table of Contents)

      • Abstract
      • 1. 서론
      • 2. LBM 유동해석법
      • 3. 해석결과
      • 4. 결론
      • Abstract
      • 1. 서론
      • 2. LBM 유동해석법
      • 3. 해석결과
      • 4. 결론
      • 참고문헌
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      참고문헌 (Reference)

      1 McNamara, G, "Use of the Boltzmann Equation to Simulate Lattice-Gas Automata" 61 : 2332-2335, 1988

      2 Zou Qisu, "On Pressure and Velocity Boundary Conditions For The Lattice Boltzmann BGK Model" 9 (9): 1591-1598, 1997

      3 Kim, H. M, "Numerical Study on Flow Over Oscillating Circular Cylinder Using Curved Moving Boundary Treatment" 31 (31): 895-903, 2007

      4 Frisch, U, "Lattice-gas Automata for The Navier-Stokes Equations" 56 : 1505-1508, 1986

      5 Qian, YH, "Lattice Gas and Lattice Kinetic Theory Apply to Navier-Stokes Equation" University et Peirre Marie Curie 1990

      6 Lallemand, P, "Lattice Boltzmann Method for Moving Boundary" 184 : 406-421, 2003

      7 Chen, S, "Lattice Boltzmann Method for Fluid Flows" 30 : 329-364, 1998

      8 Buick, JM, "Gravity in a Lattice Boltzmann Model" 61 (61): 5307-5320, 2000

      9 Mei, R, "Force Evaluation in the Lattice Boltzmann Method Involving Curved Geometry" 65 : 2002

      10 Schafer, M, "Flow Simulation with High-Performance Computer II" 52 : 547-, 1996

      1 McNamara, G, "Use of the Boltzmann Equation to Simulate Lattice-Gas Automata" 61 : 2332-2335, 1988

      2 Zou Qisu, "On Pressure and Velocity Boundary Conditions For The Lattice Boltzmann BGK Model" 9 (9): 1591-1598, 1997

      3 Kim, H. M, "Numerical Study on Flow Over Oscillating Circular Cylinder Using Curved Moving Boundary Treatment" 31 (31): 895-903, 2007

      4 Frisch, U, "Lattice-gas Automata for The Navier-Stokes Equations" 56 : 1505-1508, 1986

      5 Qian, YH, "Lattice Gas and Lattice Kinetic Theory Apply to Navier-Stokes Equation" University et Peirre Marie Curie 1990

      6 Lallemand, P, "Lattice Boltzmann Method for Moving Boundary" 184 : 406-421, 2003

      7 Chen, S, "Lattice Boltzmann Method for Fluid Flows" 30 : 329-364, 1998

      8 Buick, JM, "Gravity in a Lattice Boltzmann Model" 61 (61): 5307-5320, 2000

      9 Mei, R, "Force Evaluation in the Lattice Boltzmann Method Involving Curved Geometry" 65 : 2002

      10 Schafer, M, "Flow Simulation with High-Performance Computer II" 52 : 547-, 1996

      11 Chen, H, "Discrete Boltzmann Systems and Fluid Flow" 7 : 632-637, 1993

      12 Higuera, F, "Boltzmann Approach to Lattice Gas Simulations" 9 : 663-668, 1989

      13 He, X, "Analytic Solutions of Simple Flow and Analysis of Non-Slip Boundary Conditions for the Lattice Boltzmann BGK Model" 87 : 115-136, 1997

      14 Renwei Mei, "An Accurate Curved Boundary Treatment in the Lattice Boltzmann Method" ICASE 2000

      15 Koelman, JMVA, "A Simple Lattice Boltzmann Scheme for Navier-Stokes Fluid Flow" 15 : 603-607, 1991

      16 Bhatnagar PL, "A Model for Collision Processes in Gases. I:Small Amplitude Processes in Charged and Neutral One-Component System" 94 : 511-525, 1954

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      학술지 이력

      학술지 이력
      연월일 이력구분 이력상세 등재구분
      2023 평가예정 해외DB학술지평가 신청대상 (해외등재 학술지 평가)
      2020-01-01 평가 등재학술지 유지 (해외등재 학술지 평가) KCI등재
      2010-01-01 평가 등재학술지 유지 (등재유지) KCI등재
      2008-01-01 평가 등재학술지 유지 (등재유지) KCI등재
      2006-01-01 평가 등재학술지 유지 (등재유지) KCI등재
      2004-01-01 평가 등재학술지 유지 (등재유지) KCI등재
      2001-01-01 평가 등재학술지 선정 (등재후보2차) KCI등재
      1998-07-01 평가 등재후보학술지 선정 (신규평가) KCI등재후보
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      기준연도 WOS-KCI 통합IF(2년) KCIF(2년) KCIF(3년)
      2016 0.23 0.23 0.25
      KCIF(4년) KCIF(5년) 중심성지수(3년) 즉시성지수
      0.22 0.19 0.552 0.03
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