• 제목/요약/키워드: Boundary Condition(경계조건)

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내재적 경계조건 방법을 적용한 비정렬 격자 기반의 정상 압축성 Navier-Stokes 해석자 (AN UNSTRUCTURED STEADY COMPRESSIBLE NAVIER-STOKES SOLVER WITH IMPLICIT BOUNDARY CONDITION METHOD)

  • 백청;김민수;최선규;이승수;김철완
    • 한국전산유체공학회지
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    • 제21권1호
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    • pp.10-18
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    • 2016
  • Numerical boundary conditions are as important as the governing equations when analyzing the fluid flows numerically. An explicit boundary condition method updates the solutions at the boundaries with extrapolation from the interior of the computational domain, while the implicit boundary condition method in conjunction with an implicit time integration method solves the solutions of the entire computational domain including the boundaries simultaneously. The implicit boundary condition method, therefore, is more robust than the explicit boundary condition method. In this paper, steady compressible 2-Dimensional Navier-Stokes solver is developed. We present the implicit boundary condition method coupled with LU-SGS(Lower Upper Symmetric Gauss Seidel) method. Also, the explicit boundary condition method is implemented for comparison. The preconditioning Navier-Stokes equations are solved on unstructured meshes. The numerical computations for a number of flows show that the implicit boundary condition method can give accurate solutions.

유한 단층 모델 및 순환 경계조건을 이용한 전지구 지진해일 예측 시스템 개발 (Development of the Global Tsunami Prediction System using the Finite Fault Model and the Cyclic Boundary Condition)

  • 이준환;박은희;박순천;우승범
    • 한국해안·해양공학회논문집
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    • 제27권6호
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    • pp.391-405
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    • 2015
  • 본 연구에서는 원거리 지진해일에 대응하기 위한 기초 연구로써 유한 단층 모델과 순환 경계조건을 이용한 전지구 지진해일 예측 시스템을 제안하였다. 제안한 전지구 지진해일 예측 시스템을 2014년 칠레 지진해일에 적용하여 원거리 지진해일에 대한 대응 시스템으로써의 가능성을 검토하였다. 전지구 지진해일 예측 시스템의 경계조건, 지배방정식, 격자 크기, 단층 모델에 따른 지진해일 파고와 도달시각을 DART 부이, 조위관측소 관측 자료와 비교함으로써 유한 단층 모델과 순환 경계조건의 중요성을 확인하였다.

2D 원통형 좌표계를 위한 FDTD 방법에서 UPML과 Liao 흡수경계조건의 비교 (Comparisons between UPML and Liao's ABC in the FDTD method for 2D Cylindrical Coordinates)

  • 홍익표
    • 한국정보통신학회논문지
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    • 제11권6호
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    • pp.1054-1061
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    • 2007
  • 본 논문에서는 2D 원통형 좌표계 구조를 해석하기 위한 전자기 수치 해석 방법 중 하나인 시간영역 유한차분법(FDTD)에서 필요한 흡수경계조건으로 UPML과 Liao 흡수경계조건을 비교하였다. 일반적인 2D 직각 좌표계에서는 UPML의 성능이 Liao의 흡수경계조건보다 우수하지만, 본 논문에서 가정한 2D 원통형 좌표계에서는 Liao에 의해 제안된 고유의 흡수경계조건이 UPML과 수정된 Liao 흡수경계조건보다 우수한 것으로 나타났다. 원통형 좌표계는 축에 대해서 대칭이기 때문에 3D 구조를 2D 구조로 가정할 수 있다는 점에서 안테나를 비롯한 다양한 마이크로파 회로의 특성해석에 널리 사용될 수 있는데, 정확한 수치해석 결과를 얻기 위해서 다양한 구조에 대한 흡수경계조건들의 비교와 검증이 필요하다.

난류-캐스케이드 상호작용 소음 예측을 위한 Perfectly Matched Layer 을 이용한 내부 입/출구 정상유동 경계조건의 개발 (Development of internal inflow/outflow steady mean flow boundary condition using Perfectly Matched Layer for the prediction of turbulence-cascade interaction noise)

  • 김대환;정철웅
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2012년도 춘계학술대회 논문집
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    • pp.521-526
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    • 2012
  • It is essential for the accurate time-domain prediction of broadband noise due to turbulence-cascade interaction to develop inflow/outflow boundary conditions to satisfy the following three requirements: to maintain the back ground mean flow, to nonreflect the outgoing disturbances and to generate the specified input gust. The preceding study(1) showed that Perfectly Matched Layer (PML) boundary condition was successfully applied to absorb the outgoing disturbances and to generate the specified gust in the time-domain computations of broadband noise due to interaction of incident gust with a cascade of flat-plates. In present study, PML boundary condition is extended in order to predict steady mean flow that is needed for the computation of noise due to interaction of incident gust with a cascade of airfoils. PML boundary condition is originally designed to absorb flow disturbances superimposed on the steady meanflow in the buffer zone. However, the steady meanflow must be computed before PML boundary condition is applied on the flow computation. In the present paper, PML equations are extended by introducing source term to maintain desired mean flow conditions. The extended boundary condition is applied to the benchmark problem where the meanflow around a cascade of airfoils is predicted. These illustrative computations reveal that the extended PML equations can effectively provide and maintain the target meanflow.

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난류-캐스케이드 상호작용 소음 예측을 위한 Perfectly Matched Layer을 이용한 내부 입/출구 정상유동 경계조건의 개발 (Development of Internal Inflow/outflow Steady Mean Flow Boundary Condition Using Perfectly Matched Layer for the Prediction of Turbulence-cascade Interaction Noise)

  • 김대환;정철웅
    • 한국소음진동공학회논문집
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    • 제22권7호
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    • pp.685-691
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    • 2012
  • It is essential for the accurate time-domain prediction of broadband noise due to turbulence-cascade interaction to develop inflow/outflow boundary conditions to satisfy the following three requirements: to maintain the back ground mean flow, to nonreflect the outgoing disturbances and to generate the specified input gust. The preceding study showed that perfectly matched layer(PML) boundary condition was successfully applied to absorb the outgoing disturbances and to generate the specified gust in the time-domain computations of broadband noise due to interaction of incident gust with a cascade of flat-plates. In present study, PML boundary condition is extended in order to predict steady mean flow that is needed for the computation of noise due to interaction of incident gust with a cascade of airfoils. PML boundary condition is originally designed to absorb flow disturbances superimposed on the steady meanflow in the buffer zone. However, the steady meanflow must be computed before PML boundary condition is applied on the flow computation. In the present paper, PML equations are extended by introducing source term to maintain desired mean flow conditions. The extended boundary condition is applied to the benchmark problem where the meanflow around a cascade of airfoils is predicted. These illustrative computations reveal that the extended PML equations can effectively provide and maintain the target meanflow.

수정된 내부 에너지 비평형 1차 외삽 경계조건을 적용한 열 유동 격자 볼츠만 모델에 관한 수치적 연구 (Numerical Simulation of Thermal Lattice Boltzmann Model with a Modified In-Ternal Energy Non-Equilibrium First-Order Extrapolation Boundary Condition)

  • 정해권;김래성;이현구;이재룡;하만영
    • 대한기계학회논문집B
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    • 제31권7호
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    • pp.620-627
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    • 2007
  • In this paper, we adapt a modified internal energy non-equilibrium first-order extrapolation thermal boundary condition to the thermal lattice Boltzmann model (TLBM). This model is the double populations approach to simulate hydrodynamic and thermal fields. The bounce-back boundary condition which is a traditional boundary condition of lattice Boltzmann method has only a first order in numerical accuracy at the boundary and numerical instability. A non-equilibrium first-order extrapolation boundary condition has been verified to be of better numerical stability than the bounce-back boundary condition and this boundary condition is proved to be of second-order accuracy for the flat boundaries. The two-dimensional natural convection flow in a square cavity with Pr=0.71 and various Rayleigh numbers are simulated. The results are found to be in good agreement with those of previous studies.

혼합경계조건에 의한 수중익 해석에 관한 연구 (A Study on Lifting Problem of Hydrofoil Using Robin Boundary Condition)

  • 문일성;이창섭;김영기
    • 대한조선학회논문집
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    • 제30권3호
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    • pp.41-50
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    • 1993
  • 본 논문은 2차원 수중익 주위의 유동해석을 위하여 포텐셜을 기저로한 여러가지 패널법을 비교 한다. 각 패널에서의 특이함수의 세기는 일정하거나 선형으로 변한다고 가정하고, Neumann 및 Dirichlet의 경계조건과 함께 혼합경계조건(Robin경계조건)을 적용하여 정식화를 한후, 각 방법의 정확도를 평가 하였다. 여러가지 2차원 단면에 대한 압력분포 및 양력을 계산하고, 해석해와 비교하였다. 날카로운 뒷날과 큰 캠버값을 갖는 날개의 경우에 특히 예민하다고 알려진 날개 뒷날 부근에서의 국소오차에 대하여 집중적인 연구를 수행하였다. 비교해석 결과, 혼합 경계조건을 사용하는 정식화 방법이 가장 정확성이 높고, 수렴속도도 우수함을 밝혔다.

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비평형 1 차 외삽 경계조건을 이용한 격자 볼츠만 법의 수치적 안정성 및 정확도에 관한 연구 (A Study on the Numerical Stability and Accuracy of Lattice Boltzmann Method with Non-equilibrium first order extrapolation boundary condition)

  • 정해권;김래성;이현구;하만영
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2007년도 춘계학술대회B
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    • pp.2684-2689
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    • 2007
  • Non-equilibrium first order extrapolation boundary condition proposed by Guo et $al.^{(9)}$ proposed has a good application for complex geometries, a second order accuracy and a treatment on non-slip wall boundary condition easily. However it has a lack of the numerical stability from high Reynolds number. Guo et $al.^{(9)}$ substituted the density value of adjacent nodes for the density of boundary nodes. This procedure causes the numerical instability on the boundary. In this paper, we derived a procedure of density extrapolation and compared to previous results.

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Redistance 방정식의 경계조건이 슬로싱 문제의 level set 해석에 미치는 영향 (EFFECT OF THE BOUNDARY CONDITION OF REDISTANCE EQUATION ON THE LEVEL SET SOLUTION OF SLOSHING PROBLEM)

  • 최형권
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2009년 춘계학술대회논문집
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    • pp.165-169
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    • 2009
  • The effect of the Dirichlet boundary condition for the redistance equation of level set method on the solutionof sloshing problem is investigated by adopting four Dirichlet boundary conditions. For the solution of the incompressible Navier-Stokes equations, P1P1 four-step fractional finite element method is employed and a least-square finite element method is used for the solutions of the two hyperbolic type equations of level set method; advection and redistance equation. ALE (Arbitrary Lagrangian Eulerian) method is used to deal with a moving computational domain. It has been shown that the free surface motion in a sloshing tank is strongly dependent on the type of the Dirichlet boundary condition and the results of broken dam and sloshing problems using various Dirichlet boundary conditions are discussed and compared with the existing experimental results.

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복합재료 적층판의 유한요소 해석을 위한 효율적 경계조건 (Effective Boundary Conditions for FEM Analysis of Composite Laminates)

  • 김택현
    • 한국생산제조학회지
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    • 제7권3호
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    • pp.92-98
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    • 1998
  • This paper presents three boundary techniques which are useful for FEM analysis of composite laminates: 1) a rotational symmetric boundary technique . 2) a quasi three-dimensional boundary technique and 3) a contact boundary technique. The use of the rotational symmetric boundary technique is possible for a smaller FEM model. With the use of the quasi three-dimensional boundary tecnique. quasi three dimensional analysis of composite laminates can be performed on the conventional 3-D FEM program These techniques can readily be adopted to FEM programs.

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