• 제목/요약/키워드: Multi-block Grid Generation

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Delaunay 삼각화 기법을 활용한 다중-블록 정렬 격자의 자동 생성 기법 (Automatic Multi-Block Grid Generation Technique Based on Delaunay Triangulation)

  • 김병수
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 1999년도 추계 학술대회논문집
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    • pp.108-114
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    • 1999
  • In this paper. a new automatic multi=block grid generation technique for general 2D regions is introduced. According to this simple and robust method, the domain of interest is first triangulated by using Delaunay triangulation of boundary points, and then geometric information of those triangles is used to obtain block topology. Once block boundaries are obtained. structured grid for each block is generated such that grid lines have $C^0-continuity$ across inter-block boundaries. In the final step of the present method, an elliptic grid generation method is applied to smoothen grid distribution for each block and also to re-locale the inter-block boundaries, and eventually to achieve a globally smooth multi-block structured grid system with $C^1-continuity$.

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포텐셜 해석자를 이용한 2차원 유동의 격자 생성 연구 (A STUDY ON THE GRID GENERATION FOR TWO-DIMENSIONAL FLOW USING A POTENTIAL SOLVER)

  • 이재훈;정경진
    • 한국전산유체공학회지
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    • 제21권1호
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    • pp.36-42
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    • 2016
  • One of the obstacles on the grid generation for complex geometries with multi-block structured grids is the domain decomposition. In this paper, the domain decomposition for two-dimensional flow is studied using the flow characteristics. The potential flow equation with the source distribution on the panel surface is solved to extract the information of the flow. The current approach is applied to a two-dimensional cylinder and Bi-NACA0012 problems. The generated grids are applied to generic flow solvers and reasonable results are obtained. It can be concluded that the current methods is useful in the domain decomposition for the multi-block structured grid.

Twin-skeg형 컨테이너선 주위의 격자계 생성과 유동 해석 (Grid Generation and flow Analysis around a Twin-skeg Container Ship)

  • 박일룡;김우전;반석호
    • 대한조선학회논문집
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    • 제41권1호
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    • pp.15-22
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    • 2004
  • Twin-skeg type stern shapes are recently adopted for very large commercial ships. However it is difficult to apply a CFD system to a hull form having twin-skeg, since grid topology around a twin-skeg type stern is more complicated than that of a conventional single-screw ship, or of an open-shaft type twin-screw ship with center-skeg. In the present study a surface mesh generator and a multi-block field grid generation program have been developed for twin-skeg type stern. Furthermore, multi-block flow solvers are utilized for potential and viscous flow analysis around a twin-skeg type stern The present computational system is applied to a 15,000TEU container ship with twin-skeg to prove the applicability. Wave profiles and wake distribution are calculated using the developed flow analysis tools and the results are compared with towing tank measurements.

상호 대화형 격자생성 환경을 이용한 항공기 전기체 격자계 생성 (Grid Generation about Full Aircraft Configuration Using Interactive Grid Generator)

  • 김윤식;권장혁
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 1999년도 추계 학술대회논문집
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    • pp.145-151
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    • 1999
  • An Interactive grid generation program(KGRID) with graphical user interface(GUI) has been improved. KGRID works on the UNLX environment and GUI has been implemented with OSF/Motif and X Toolkit and the graphics language is Open GL for visualization of the 3D objects. It supports more convenient user environment to generate 2D and 3D multi-block structured grid systems. It provides various useful field grid generation methods, which are the algebraic methods, the elliptic partial differential equations method and the predictor-corrector method. It also supports 3D surface grid generation with NURBS(Non-Uniform Rational B-Spline) and various stretching functions to control grid points distribution on curves and surfaces. And some menus are added to perform flexible management, for the objects. We generated surface and field grid system about full aircraft configuration using KGRID. The performance and stability of the KGRID is verified through the generation of the grid system about a complex shape.

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2차원 유동 해석을 위한 OpenFOAM용 격자 생성 프로그램 개발 (DEVELOPMENT OF OPENFOAM GRID GENERATION PROGRAM FOR TWO-DIMENSIONAL FLOW ANALYSIS)

  • 김왕현;김병수
    • 한국전산유체공학회지
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    • 제21권2호
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    • pp.25-31
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    • 2016
  • In this paper, a study on the development of OpenFOAM grid generation program for two-dimensional flow analysis is described. By using the pre-processor(eMEGA) of EDISON_CFD system, grids for OpenFOAM flow calculation were obtained. Resultant two-dimensional grids were used to calculate flow fields by applying simpleFoam, one of the OpenFOAM's popular solvers, and the obtained flow results were compared with theoretical and experimental data available. Also grids generated by present program were compared with grids by a commercial pre-processor Pointwise for the purpose of verification. Verification work includes three cases(single block, O-type single block, and multi block grid), and all results show reasonable matches. According to the current achievement, it can be concluded that OpenFOAM grid can be constructed conveniently by using eMEGA with GUI.

축류압축기의 공력설계를 위한 대화형 계산격자점 생성 프로그램 개발 (Interactive System of Computational Grid Generation for Aerodynamic Design of Axial Flow Compressors)

  • 정희택
    • 한국유체기계학회 논문집
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    • 제1권1호
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    • pp.7-16
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    • 1998
  • An interactive mode of grid generation system has been developed for a Navier-Stokes design procedure of axial flow compressors. The present grid generator adopts the multiblock H-grid structure, which simplifies the creation of computational grids about complex turbomachinery geometries and facilitate the manipulation of multiple grid blocks for multirow flow fields. The numerical algorithm adopts the combination of the algebraic and elliptic method to create the internal grids efficiently and quickly. The system consists of four separated modules, which are linked together with a common graphical user interface. The system input is made of the results of the preliminary design. The final grids generated from each module of the system are used as the preprocessor for the performance prediction of the two-or three-dimensional flow simulation inside the blade passage. Application to the blade design of the LP compressor was demonstrated to be very reliable and practical in support of design activities. This customized system are coupled strongly with the design procedure of the turbomachinery cascades using the Navier-Stokes technique.

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다중 GPU기반 홀로그램 생성을 위한 병렬처리 성능 최적화 기법 (An Optimization Method for Hologram Generation on Multiple GPU-based Parallel Processing)

  • 국중진
    • 스마트미디어저널
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    • 제8권2호
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    • pp.9-15
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    • 2019
  • 홀로그램의 생성을 위한 연산은 포인트 클라우드의 규모에 따라 연산량이 기하급수적으로 증가하기 때문에 최근에는 다중의 GPU를 기반으로 CUDA 또는 OpenCL 라이브러리를 활용한 병렬처리가 이루어지고 있다. GPU기반의 병렬처리를 위한 CUDA 커널은 GPU의 코어 개수와 메모리 크기를 고려하여 쓰레드(thread), 블록(block), 그리드(grid)를 구성해야 하며, 다중 GPU 환경인 경우 GPU의 개수에 따른 그리드, 블록, 또는 쓰레드 단위의 분산처리가 필요하다. 본 논문에서는 CGH 생성에 대한 성능평가를 위해 포인트 클라우드의 포인트 개수를 10~1,000,000개 범위에서 점진적으로 증가시키면서 CPU, 단일 GPU, 다중 GPU 환경에서 연산 속도를 비교해 보았으며, 다중 GPU 환경에서 CGH(Computer Generated Hologram) 생성 연산을 가속화하기 위한 CUDA 기반의 병렬처리 과정에서 요구되는 메모리 구조 설계와 연산 방법을 제안한다.

2차원 지면 효과에 대한 난류 유동장 해석 Part I. 중첩 격자 기법 적용에 대한 연구 (Turbulent Flow Simulations on 2-Dimensional Ground Effect Part I. Verification on the Overlap Grid Method)

  • 김윤식;이재은;김유진;권장혁
    • 한국항공우주학회지
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    • 제35권8호
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    • pp.661-669
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    • 2007
  • 지면효과에 대한 수치해석을 위한 격자생성 과정에서 발생하는 어려움을 해소하기 위하여 중첩격자 기법을 이용한 수치해석 기법의 타당성에 대한 연구를 수행하고 그 신뢰성을 검증하였다. 지면효과가 있는 경우와 없는 경우 RAE 101 익형주위의 저속 난류 유동장에 대한 수치해석을 수행하였고 다중블록격자 기법과 중첩격자 기법을 적용한 수치해석 결과를 실험결과와 비교하였다. 이를 통하여 중첩격자 기법을 이용함으로써 지면효과에 대한 수치해석과정을 정확하고 격자생성 문제없이 효과적으로 수행할 수 있음을 보였다.

진동하는 2차원 날개 단면 주위에 대한 점성 유동장 계산( Part 1. 동적실속이 없는 경우 ) (Computation of Viscous Flows around a Two-dimensional Oscillating Airfoil ( Part 1. without Dynamic Stall ))

  • 이평국;김형태
    • 대한조선학회논문집
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    • 제44권1호
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    • pp.8-15
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    • 2007
  • In this paper, numerical calculations are performed to analyze the unsteady flow of NACA airfoil sections. In order to ease the flow computation for the fluid region changing in time, improve the quality of solution and simplify the grid generation for the oscillating foil flow, the computational method adopts a moving and deforming mesh with the multi-block grid topology. The multi-block, structured-unstructured hybrid grid is generated using the commercial meshing software Gridgen V15. The MDM (Moving & Deforming Mesh) and the UDF (User Define function) function of FLUENT 6 are adopted for computing turbulent flows of the foil in pitching motion. Computed unsteady lift and drag forces are compared with experimental data. in general, the characteristics of unsteady lift and drag of the experiments are reproduced well in the numerical analysis.

중첩 격자계를 이용한 물체운동의 수치 시뮬레이션 (Numerical Simulation of Body Motion Using a Composite Grid System)

  • 박종천;전호환;송기종
    • 대한조선학회논문집
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    • 제40권5호
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    • pp.36-42
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    • 2003
  • A CFD simulation technique has been developed to handle the unsteady body motion with large amplitude by use of overlapping multi-block grid system. The three-dimensional, viscous and incompressible flow around body is investigated by solving the Navier-Stokes equations, and the motion of body is represented by moving effect of the grid system. Composite grid system is employed in order to deal with both the body motion with large amplitude and the condition of numerical wave maker in convenience at the same time. The governing equations, Navier-Stokes (N-S) and continuity equations, are discretized by a finite volume method, in the framework of an O-H type boundary-fitted grid system (inner grid system including test model) and a rectangular grid system (outer grid system including simulation equipments for generation of wave environments). If this study, several flow configurations, such as an oscillating cylinder with large KC number, are studied in order to predict and evaluate the hydrodynamic forces. Furthermore, the motion simulation of a Series 60 model advancing in a uniform flow under the condition of enforced roll motion of angle 20$^{\circ}$ is performed in the developed numerical wave tank.