• 제목/요약/키워드: Flow computation

검색결과 981건 처리시간 0.023초

Analyses of Computation Time on Snakes and Gradient Vector Flow

  • Kwak, Young-Tae
    • Journal of the Korean Data and Information Science Society
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    • 제18권2호
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    • pp.439-445
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    • 2007
  • GVF can solve two difficulties with Snakes that are on setting initial contour and have a hard time processing into boundary concavities. But GVF takes much longer computation time than the existing Snakes because of their edge map and partial derivatives. Therefore this paper analyzed the computation time between GVF and Snakes. As a simulation result, both algorithms took almost similar computation time in simple image. In real images, GVF took about two times computation than Snakes.

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Eulerian-Lagrangian 방법에서 입자 및 유동 격자계 분리를 통한 2상 유동의 효율적 계산 (Efficient Computation of Two-Phase Flow by Eulerian-Lagrangian Method Using Separate grids for the Particles and Flow Field)

  • 박순일;이진규;장근식
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2003년도 추계 학술대회논문집
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    • pp.43-48
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    • 2003
  • When the Eulerian-Lagrangian method is used to analyze the particle laden two-phase flow, a large number of particles should be used to obtain statistically meaningful solutions. Then it takes too much time to track the particles and to average the particle properties in the numerical analysis of two-phase flow. The purpose of this paper is to reduce the computation time by means of a set of particle gird separate to the flow grid. Particle motion equation here is the simplified B-B-O equation, which is integrated to get the particle trajectories. Particle turbulent dispersion, wall collision, and wall roughness effects are considered but the two-way coupling effects between gas and particles are neglected. Particle laden 2-D channel flow is solved and it is shown that the computational efficiency is indeed improved by using the current method

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사각덕트내의 유체유동에 관한 수치계산과 실험의 비교 (The comparison between Numerical Computation and Experiment on Fluid Elow in Rectangular Duct)

  • 윤영환;배택희;박원구
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2002년도 학술대회지
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    • pp.71-74
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    • 2002
  • Fluid flow in a rectangular duct system are measured by W laser doppler velocity meter, and also computed by commercial software of STAR-CD for comparison between then First, for a rectangular duct with 90 degree metered elbow, the fluid flow with Reynolds numbs's of 1,508 is predicted by assumption of both laminar and turbulent models. But, even though the Reynolds number is less than 2,300-3,000, the computation by turbulent model is close to the experimental data. Moeover, the computation by turbulent model for Reynolds number of 11,751 also predicts the experimental data satisfactorily. Second, for a rectangular duct with two branch ducts, the ratios between flow rates in the two branches are invariant to Reynolds number according to both of numerical and experimental results.

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Self-timed 기반의 Node Label Data Flow Machine 설계 (Design of a Node Label Data Flow Machine based on Self-timed)

  • 김희숙;정성태;박희순
    • 대한전기학회:학술대회논문집
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    • 대한전기학회 1998년도 추계학술대회 논문집 학회본부 B
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    • pp.666-668
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    • 1998
  • In this paper we illustrate the design of a node label data flow machine based on self-timed paradigm. Data flow machines differ from most other parallel architectures, they are based on the concept of the data-driven computation model instead of the program store computation model. Since the data-driven computation model provides the excution of instructions asynchronously, it is natural to implement a data flow machine using self timed circuits.

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사각덕트내 직각엘보우를 지난 유체유동에 관한 연구 (Study on Fluid Flow in Rectangular Duct past $90^{\circ}$ Mitered Elbow)

  • 윤영환;배택희;박원구
    • Journal of Advanced Marine Engineering and Technology
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    • 제26권6호
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    • pp.670-678
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    • 2002
  • Fluid flow in a rectangular duct with $90^{\circ}$ mitered elbow is measured by 5W laser doppler velocity meter. The fluid flow is also computed by commercial software of STAR-CD for comparison between measured and computed velocity profiles in the duct. Reynolds numbers for the comparison are 1,608 and 11,751 based on mean velocity and hydraulic diameter of the duct. First, the fluid flow of Reynolds number equal to 1,608 is predicted by assumptions of both laminar and turbulent models. But, even though the Reynolds number is less than 2,300~3,000, the computation by turbulent model is closed to the experimental data than that by laminar model. Second, the computation for Reynolds number of 11,751 by turbulent model also predicted the experimental data satisfactorily.

경계조건에 따른 공력음향 특성에 관한 연구 (THE STUDY OF AERO-ACOUSTICS CHARACTERISTIC BY BOUNDARY CONDITIONS)

  • 이상수;김재수
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2009년 춘계학술대회논문집
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    • pp.75-80
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    • 2009
  • The present paper focuses on the analysis of aero-acoustics characteristic by several boundary conditions. In this simulation, a high-order and high-resolution numerical schemes are used for the accurate computation of compressible flow with several boundary conditions including characteristic boundary conditions as well as extrapolation and zonal characteristic boundary condition. These boundary conditions are applied to the computation of two dimensional circular cylinder flows with Mach number of 0.3 and Reynolds number of 400. The computation results are validated with measurement datum and other computation results for the Strouhal frequency of vortex shedding, the mean drag coefficient and root-mean-square lift for the unsteady periodic flow regime. Secondary frequency is predicted by three kinds of boundary conditions characteristic.

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SPARSE NULLSPACE COMPUTATION OF EQULILBRIUM MATRICES

  • Jang, Ho-Jong;Cha, Kyung-Joon
    • 대한수학회논문집
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    • 제11권4호
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    • pp.1175-1185
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    • 1996
  • We study the computation of sparse null bases of equilibrium matrices in the context of structural optimization and incompressible fluid flow. In our approach we emphasize the parallel computatin and examine the applications. New block decomposition and node ordering schemes are suggested, and numerical examples are considered.

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이완 결합형 다중 프로세서 시스템을 사용한 데이터 플로우 컴퓨터 구조의 병렬 에뮬레이션에 관 한 연구 (A Parallel Emulation Scheme for Data-Flow Architecture on Loosely Coupled Multiprocessor Systems)

  • 이용두;채수환
    • 한국통신학회논문지
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    • 제18권12호
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    • pp.1902-1918
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    • 1993
  • 노이만 계산 모델의 병렬처리 구조는 구조 속성상의 취약성으로 인해 대량 병렬처리 구조로서는 한계가 있다. 데이터 플로우 계상 모델은 소프트웨어적 고 프로그램성과 하드웨어적 높은 개발 가능성을 갖고 있다. 그러나 실제 데이터 플로우 구조에서는 프로그래밍과 실험을 행하고자 할때, 노이만 방식의 기계는 많지만 실제 데이터 플로우 컴퓨터가 없으므로 대단히 어렵다. 본 논문에서는 일반적 재래 병렬처리기계중 하나인 이완결합 다중프로세서 시스템위에서 데이터 플로우 방식의 계산을 수행시킬 수 있는 프로그래밍 환경을 제시하였다. 에뮬레이터는 iPSC/2 하이퍼 큐프를 이용하여 Tagged Token 데이터 플로우 구조를 구축하였다. 본 에뮬레이터는 iPSC/2시스템에서 소프트웨어적 박층 실험으로 프로그래머의 입장에서는 iPSC/2 시스템이 데이터 플로우 주고로서 농작하는 것으로 간주한다. 여러 가지 수치 혹은 비수치 알고리즘을 데이터 플로우 어셈블리어로 구현하여 재래식 C 언어에 의한 것과 프로그램의 성능을 비교하였다. 이로써, 재래식 병렬처리 기계상의 에뮬레이터를 통한 실험적 데이터 플로우 계산을 행할 때 이 프로그래밍 환경의 효율성에 대하여도 검정하였다.

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외부유동에 의한 캐버티 내의 비정상 유동에 대한 수치계산 (Numerical Computation of Unsteady Flow in a Cavity Induced by an Oscillatory External Flow)

  • Yong kweon Suh;Park, Yoon-Hwan;Park, Jun-Gwan;Moon, Jong-Ghoon
    • 한국해안해양공학회지
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    • 제9권4호
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    • pp.194-200
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    • 1997
  • 주기적으로 요동하는 외부유동에 의해 생성되는 캐버티 주위의 2차원 천수유동은 수치적으로 연구하였다. 실험결과와 비교하기 위해 T형의 용기모델을 수치적으로 계산하여 만들었다. 수치계산에서는 캐버티의 종횡비가 전체적인 유동패턴에 크게 영향을 끼치지 않고 종횡비 2에서는 캐버티의 깊은 부분에 정체된 유동형태가 생성되는 것을 제시한다. 높은 레이놀즈 수에서 유동을 가시화 시켰을 때 나다나지 않았던 많은 와류들이 유동장을 특성화 시키고 있다. 외부지역에서의 물질전달은 실험에서 나타난 입자궤적과 잘 일치한다. 캐버티의 외부지역에 위치한 두쌍의 와류가 규모가 큰 시계방향과 반시계방향의 순환유동을 발생시키는 원인이 되는 것이 증명된 셈이다.

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병렬계산에 의한 비축대칭 3차원 스핀업 유동해석 (Analysis of Three-dimensional Nonaxisymmetric Spin-up by Using Parallel Computation)

  • 박재현;최윤환;서용권
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2001년도 춘계학술대회논문집E
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    • pp.512-517
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    • 2001
  • In this study, spin-up flows in a rectangular container are analysed by using three-dimensional computation. In the numerical computation, we use the parallel computer system of PC-cluster type. We compared our results with those obtained by two-dimensional computation. Effect of velocity and vorticity on the flow is studied. The result shows that two-dimensional solution is in good agreement with the 3-D result. Attention is given to the region where the 3-D flow is significant.

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