• 제목/요약/키워드: Computational study

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계산 그리드를 위한 서비스 예측 기반의 작업 스케쥴링 모델 (Service Prediction-Based Job Scheduling Model for Computational Grid)

  • 장성호;이종식
    • 한국시뮬레이션학회:학술대회논문집
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    • 한국시뮬레이션학회 2005년도 춘계학술대회 논문집
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    • pp.29-33
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    • 2005
  • Grid computing is widely applicable to various fields of industry including process control and manufacturing, military command and control, transportation management, and so on. In a viewpoint of application area, grid computing can be classified to three aspects that are computational grid, data grid and access grid. This paper focuses on computational grid which handles complex and large-scale computing problems. Computational grid is characterized by system dynamics which handles a variety of processors and jobs on continuous time. To solve problems of system complexity and reliability due to complex system dynamics, computational grid needs scheduling policies that allocate various jobs to proper processors and decide processing orders of allocated jobs. This paper proposes the service prediction-based job scheduling model and present its algorithm that is applicable for computational grid. The service prediction-based job scheduling model can minimize overall system execution time since the model predicts a processing time of each processing component and distributes a job to processing component with minimum processing time. This paper implements the job scheduling model on the DEVSJAVA modeling and simulation environment and simulates with a case study to evaluate its efficiency and reliability Empirical results, which are compared to the conventional scheduling policies such as the random scheduling and the round-robin scheduling, show the usefulness of service prediction-based job scheduling.

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이동 벽면에 의한 원형 실린더의 비대칭적 공력 발달에 관한 전산연구 (A COMPUTATIONAL STUDY ABOUT THE ASYMMETRIC AERODYNAMIC EVOLUTION AROUND A CIRCULAR CYLINDER CAUSED BY A MOVING WALL)

  • 정재윤;장조원
    • 한국전산유체공학회지
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    • 제11권3호
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    • pp.64-70
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    • 2006
  • A Computational study was carried out in order to investigate the moving wall effect of a circular cylinder at a Reynolds number of $2.0{\times}10^4$. The viscous-incompressible Navier-Stokes equations and Spalart-Almaras turbulent model of the commercial CFD code were adopted for this numerical analysis. The moving wall was set parallel with the freestream, and moving speed was equal to the freestream velocity. The gap ratio is defined as the distance ratio between the circular cylinder diameter and the height from the moving wall. The results show that there is vortex shedding over the critical gap ratio and aerodynamic loads including amplitude and the Strouhal number change according to the gap ratio.

공작기계의 정밀도 향상을 위한 전산 메카트로닉스 해석 (Computational Mechatronics Analysis to Design High Precision N.C. Machine)

  • 김동현;김동만;박강균
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2008년도 추계학술대회논문집
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    • pp.205-209
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    • 2008
  • In this study, very accurate computational mechatronics method has been developed for typical N.C. machine model applying to manufacturing industry in these days. Computation analysis of high speed machine tools like N.C. machine needs consideration about mechatronical features because the machine shows close interaction between dynamic behavior of the mechanical structure, drives and numerical control. For this, nonlinear structural analysis tools based on FEM are linked numerical control program to control the dynamic behavior. In this study, we studied the dynamic feature of N.C. machine by using SAMCEF as nonlinear computational structural analysis tool and simulink as drivers.

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이원자 기체 유동 해석을 위한 일반유체역학 계산모델 개발 (Generalized Hydrodynamic Computational Models for Diatomic Gas Flows)

  • 명노신;조수용
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2001년도 춘계 학술대회논문집
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    • pp.111-115
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    • 2001
  • The study of nonlinear gas transport in rarefied condition or associated with the microscale length of the geometry has emerged as an interesting topic in recent years. Along with the DSMC method, several fluid dynamic models that come under the general category of the moment method or the Chapman-Enskog method have been used for this type of problem. In the present study, on the basis of Eu's generalized hydrodynamics, a computational model for diatomic gases is proposed. The preliminary result indicates that the bulk viscosity plays a considerable role in fundamental flow problems such as the shock structure and shear flow. The general properties of the constitutive equations are obtained through a simple mathematical analysis. With an iterative computational algorithm of the constitutive equations, numerical solutions for the multi-dimensional problem can be obtained.

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유체$\cdot$구조물 상호 작용 기법을 이용한 오일 펜스의 변형 예측 (Prediction of Deformation of an Oil-fence by using Fluid$\cdot$Structure Interaction Method)

  • 김태균;김욱;허남건
    • 한국전산유체공학회지
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    • 제5권3호
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    • pp.16-22
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    • 2000
  • In the present study a method of computing fluid-structure interaction is presented to simulate the deformation shape of an oil fence which is used to contain or to divert the split oil in sea water. The computation is performed by taking into account of the force and moment balance in each computational element of the oil fence. The forces and moments acting on each element of the structure is computed from the flow analysis, which in turn is used to predict deformed shape of the structure until the procedure converges. The flexibility of the oil fence was also considered in the analysis. It is shown from the present study that the predicted deformed shapes agree quite well with the available experiment data.

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미사일 단분리 시스템의 비정상 유동장 해석 (NUMERICAL SIMULATION OF UNSTEADY MISSILE STAGING SYSTEM)

  • 윤용현;권기범;홍승규
    • 한국전산유체공학회지
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    • 제10권4호통권31호
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    • pp.24-31
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    • 2005
  • A dynamic simulation on the missile staging system is conducted with numerical techniques. Both Euler equations and Navier-Stokes equations are numerically solved respectively. The dynamic simulation of two moving bodies is fully integrated into the computational fluid dynamics solution procedure. The Chimera grid scheme is applied in this simulation for unsteady supersonic flow analysis with dynamic modeling. The objective of the study is to investigate the problem pertaining to possible unstability in missile staging. In addition, the computational comparison between in viscid and viscid flow solvers is also performed in this study.

NURBS를 이용한 격자생성 및 제어기법 (A STUDY ON THE NURBS GRID GENERATION AND GRID CONTROL)

  • 윤용현
    • 한국전산유체공학회지
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    • 제12권3호
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    • pp.20-28
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    • 2007
  • A fast and robust method of grid generation to multiple functions has been developed for flow analysis in three dimensional space. It is based on the Non-Uniform Rational B-Spline(NURBS) of an approximation method. Many of NURBS intrinsic properties are introduced and much more easily understood. The grid generation method, details of numerical implementation. examples of application, and potential extensions of the current method are illustrated in this paper. The object of this study is to develop the surface grid generation and the grid cluster techniques capable of resolving complex flows with shock waves, expansion waves, shear layers. The knot insert method of Non-Uniform Rational B-Spline seems well worked. In addition, NURBS has been widely utilized to generate grids in the computational fluid dynamics community. Computational examples associated with practical configurations have shown the utilization of the algorithm.

근사신뢰도기법을 이용한 효율적인 공력 형상 설계에 관한 연구 (Study of the Efficient Aerodynamic Shape Design Optimization Using the Approximate Reliability Method)

  • 김수환;권장혁
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2004년도 추계 학술대회논문집
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    • pp.187-191
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    • 2004
  • The conventional reliability based design optimization(RBDO) methods require high computational cost compared with the deterministic design optimization(DO) methods. To overcome the computational inefficiency of RBDO, single loop methods have been proposed. These need less function calls than that of RBDO but much more than that of DO. In this study, the approximate reliability method is proposed that the computational requirement is nearly the same as DO and the reliability accuracy is good compared with that of RBDO. Using this method, the 3-D viscous aerodynamic shape design optimization with uncertainty is performed very efficiently.

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터보펌프 인듀서에 대한 수치해석적 연구 (NUMERICAL STUDY ON THE TURBOPUMP INDUCER)

  • 노준구;최창호;홍순삼;김진한
    • 한국전산유체공학회지
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    • 제11권1호
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    • pp.16-20
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    • 2006
  • The present study focuses on the flow analysis of a turbo pump inducer by performing both numerical and experimental methods. The head rise, efficiency and detailed flow fields such as outlet flow angles, pressure and velocity vectors are measured and compared with the computational data. Generally a good agreement is obtained between numerical and experimental results. However, some discrepancies are observed due to complex flow structures inside the inducer. Future calculations with an advanced turbulence model and a dense computational grid needs to be performed to obtain accurate numerical solution for the detailed flow fields.

인터넷을 활용하기 위한 수치해석 프로그램의 재구성 방법 (Reconstructing Methods of Numerical Analysis Program for Utilizing the Internet)

  • 송희용;고성호
    • 한국전산유체공학회지
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    • 제8권1호
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    • pp.16-22
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    • 2003
  • The present study introduces an architecture for performing efficient numerical analysis by using the Internet and three reconstructing methods of existing numerical analysis codes were presented in order to utilize the architecture. These methods were implemented into a computational fluid dynamics program for solving two-dimensional transient flow problems with free surface. The program was reconstructed with Java technologies and compared with the original one. This study will be a preparation for numerical analysis to participate in web services for engineering.