• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2009년도 제33회 추계학술대회논문집
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• pp.329-334
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• 2009

형상에 따른 오리피스의 동특성을 확인하기에 앞서 정상 상태에서의 성능에 대한 연구가 선행되어야 한다. 이를 위해 수치해석을 통해 개도, 두께, 팽창각에 따른 오리피스의 성능을 예측하였다. 유동 해석 알고리듬은 SIMPLEC을 사용하였고, 차분 기법은 PRESTO, QUICK 기법을 사용하였으며, 난류 모델은 $k-{\omega}$ STS를 사용하였다. 오리피스의 개도가 증가하면서 유량계수는 급격하게 증가하였고, 두께가 증가하면서 유량계수는 급격하게 증가하였다가 서서히 감소한다. 팽창각이 45도일 때 유량계수가 가장 작게 나타났다.

• 대한조선학회논문집
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• 제37권4호
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• pp.19-30
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• 2000

선수와 선미에 벌브를 가진 현대적인 상선 주위의 난류유동을 해석하기 위해 유한체적법을 이용한 RANS 방정식의 해법이 개발되었다. 복잡한 선수미의 격자계 생성을 위해 다중블록 선체표면 격자계 생성 기법이 도입되었고, 타원형 미분 방정식의 해를 이용하여 O-H 형태의 공간 격자계생성 기법이 이용되었다. 지배방정식의 대류항과 확산항은 각각 QUICK과 중앙차분법을 이용하여 근사되었고, 속도-압력 연성을 위해 SIMPLEC법이 채택되었다. 개발된 방법은 KRISO 3600TEU 컨테이너선에 적용하여 유선가시화 실험 및 반류계측 결과와 비교하였다. 계산 결과는 선수와 선미에 벌브를 가진 현대적인 선형 주위의 유동 해석을 위해서도 이러한 수치계산 방법이 적용될 수 있음을 보여주고 있다.

• 에너지공학
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• 제2권3호
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• pp.268-275
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• 1993

수치해석 방법에 의해 큐백시의 스토커 소각로 유동장을 분석하였다. 수치모사의 변수는 큐백시의 스토커 소각로를 중심으로 한 5가지 내부 형상, 1차공기 속도, 2차공기 속도 및 주입각, 출구면적을 고려하였다. 검사체적에 기초한 Patankar의 유한차분 방법을 사용한 본 논문에서는 power-law scheme과 SIMPLEC 알고리즘을 사용했으며 난류 유동은 표준 k-e 모델을 이용했다. 소각로 유동장 분석을 위해서 재순환 영역의 크기, 난류 점성계수 및 이차공기의 질량분율 분포, 압력강하를 계산했다. 계산 결과는 물리적 의미에 잘 맞게 나타났으며, 큐백시의 스토커 소각로가 다른 내부 형상의 소각로에 비해 상부에 강한 난류를 가진 재순환 영역을 형성하였다.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2008년도 학술대회
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• pp.1-13
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• 2008

An efficient segregated algorithm for the coupling of velocity and pressure of incompressible fluid flow, called IDEAL Inner Doubly-Iterative Efficient Algorithm for Linked-Equations), has been proposed by the present authors. In the algorithm there exist double inner iterative processes for pressure equation at each iteration level, which almost completely overcome two approximations in SIMPLE algorithm. Thus the coupling between velocity and pressure is fully guaranteed, greatly enhancing the convergence rate and stability of solution process. The performance of the IDEAL algorithm for three-dimensional incompressible fluid flow and heat transfer problems is analyzed and a systemic comparison is made between the algorithm and three other most widely-used algorithms (SIMPLER, SIMPLEC and PISO). It is found that the IDEAL algorithm is the most robust and the most efficient one among the four algorithms compared. This new algorithm is used for the velocity prediction of a new interface capturing method. VOSET, also proposed by the present author. It is found that the combination of VOSET and IDEAL can appreciably enhance both the interface capture accuracy and convergence rate of computations.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2008년 추계학술대회논문집
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• pp.1-13
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• 2008

An efficient segregated algorithm for the coupling of velocity and pressure of incompressible fluid flow, called IDEAL (Inner Doubly-Iterative Efficient Algorithm for Linked-Equations), has been proposed by the present authors. In the algorithm there exist double inner iterative processes for pressure equation at each iteration level, which almost completely overcome two approximations in SIMPLE algorithm. Thus the coupling between velocity and pressure is fully guaranteed, greatly enhancing the convergence rate and stability of solution process. The performance of the IDEAL algorithm for three-dimensional incompressible fluid flow and heat transfer problems is analyzed and a systemic comparison is made between the algorithm and three other most widely-used algorithms (SIMPLER, SIMPLEC and PISO). It is found that the IDEAL algorithm is the most robust and the most efficient one among the four algorithms compared. This new algorithm is used for the velocity prediction of a new interface capturing method -VOSET, also proposed by the present author. It is found that the combination of VOSET and IDEAL can appreciably enhance both the interface capture accuracy and convergence rate of computations.

• 에너지공학
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• 제5권1호
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• pp.50-55
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• 1996

상용 code인 Fluent를 이용하여 도자기의 1차 소성로에 대해 온도장과 속도장을 계산하고 열효율을 산출하였다. 수치해석의 변수로는 배출구 및 도자기의 위치를 변화시켰으며, 수치해석 방법은 검사체적에 기초한 유한차분방법 및 Upwind scheme과 SIMPLEC Algorithm을 사용하였고 난류모델로는 표준 k-$\varepsilon$ 모델을 사용하였다. 계산결과 출구 위치가 전체 소성로내 벡터유동의 양상을 크게 좌우하는 것으로 나타났으며, 전체 온도장에 대해서는 복사의 영향으로 큰 차이를 보이지 않았으나 예열대 상부에 출구가 있는 경우와 비교할 때 예열대 또는 냉각대의 측면에 출구가 있는 경우에 그 영역의 온도가 다소 높게 나타났다. 소성품의 위치는 로내 유동장 및 온도 분포에 크게 영향을 끼치지는 않으나 소성품 내 온도는 그 위치하는 영역의 온도 분포에 크게 영향을 받는 것으로 나타났다. 예열대 상부에 출구가 있는 경우 열효율은 17%로 매우 저조하였고 출구에서의 가스온도는 약 1000 K로 매우 높았다.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2001년도 춘계학술대회논문집E
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• pp.684-689
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• 2001

In this study, three-dimensional viscous flow analysis and optimization are presented for the design of a mixed-flow fan. Steady, imcompressible, three-dimensional Reynolds averaged Navier-Stokes equations are used as governing equations, and standard $k-{\varepsilon}$ turbulence model is chosen as a turbulence model. Governimg equations are discretized using finite volume method. Upwind difference scheme is used for the discretization of the convective term and SIMPLEC algorithm is used as a velocity-pressure correction procedure. The computational results are compared with the results obtained by TASCflow. For the numerical optimization of the design, objective function is defined as a ratio of generation of the turbulent energy to pressure head. Sweep angles are used as design variables.

• 한국안전학회지
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• 제9권1호
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• pp.146-154
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• 1994

A series of numerical calculations are performed in order to investigate the dispersion mechanism of toxic gaseous and solid pollutants in extremely short-term and short range. The calculations are carried out in an open space characterized by turbulent boundary layer. The simulation is made by the use of numerical model, in which a control-volume based finite difference method is used together with the SIMPLEC algorithm for the resolution of the pressure-velocity coupling problem. The Reynolds stresses are solved by two-equation, k-$\varepsilon$ model modified for buoyancy. The major parameters consider-ed in this study are temperature, velocity and Injection height of toxic gases, environmental conditions such as temperature and velocity of free stream air, and topographic factor. The results are presented and discussed in detail. The flow field is commonly characterized by the formation of a strong recirculation zone due to the upward motion of the hot toxic gas and ground shear stress. The driving force of the upward motion is explained by the effect of thermal buoyancy of hot gas and the difference of inlet velocity between toxic gas and free stream.

• 한국전산유체공학회지
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• 제10권4호통권31호
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• pp.1-11
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• 2005

A numerical study of the evaluation of turbulence models for thermal striping phenomenon is performed. The turbulence models chosen in the present study are the two-layer model, the shear stress transport (SST) model and the V2-f model. These three models are applied to the analysis of the triple-jet flow with the same velocity but different temperatures. The unsteady Reynolds-averaged Navier-Stokes (URANS) equation method is used together with the SIMPLEC algorithm. The results of the present study show that the temporal oscillation of temperature is predicted by the SST and V2-f models, and the accuracy of the mean velocity, the turbulent shear stress and the mean temperature is a little dependent on the turbulence model used. In addition, it is shown that both the two-layer and SST models have nearly the same capability predicting the thermal striping, and the amplitude of the temperature fluctuation is predicted best by the V2-f model.

• Advances in Energy Research
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• 제1권1호
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• pp.53-78
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• 2013

Methane carbon dioxide reforming (MCDR) is a promising way of utilizing greenhouse gas for hydrogen-rich fuel production. Compared with other types of reactors, Compact Reformers (CRs) are efficient for fuel processing. In a CR, a thin solid plate is placed between two porous catalyst layers to enable efficient heat transfer between the two catalyst layers. In this study, the physical and chemical processes of MCDR in a CR are studied numerically with a 2D numerical model. The model considers the multi-component gas transport and heat transfer in the fuel channel and the porous catalyst layer, and the MCDR reaction kinetics in the catalyst layer. The finite volume method (FVM) is used for discretizing the governing equations. The SIMPLEC algorithm is used to couple the pressure and the velocity. Parametrical simulations are conducted to analyze in detail the effects of various operating/structural parameters on the fuel processing behavior.