• 한국수자원학회논문집
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• 제32권3호
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• pp.225-235
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• 1999

가로흐름이 존재하는 수역으로 방출되는 온배수 해석에 3가지 난류모형의 사용성 평가를 위해서 근역 2차원 수치모형을 개발하였다. 적용한 난류모형은 2-방정식 난류모형인 {{{{ { k}_{ } }}}}-$\varepsilon$ 및 {{{{ { k}_{ } }}}}-ι 난류모형과 {{{{ { k}_{ } }}}}-$\varepsilon$ 난류모형에 부력생성 항 및 난류 열 플럭스 항 결정을 위한 변동온도 평균자승항 및 이의 감쇠율에 대한 전달 방정식을 추가한 4-방정식 난류모형이다. 개발된 모형은 간단한 단면을 갖는 개수로 정류 경우에 대해 적용하였으며, 계산된 결과는 기존의 실험결과와 비교적 잘 일치하였다. 4-방정식 난류모형에 의한 결과가 2-방정식에 의한 결과보다 부력에 의한 횡방향의 중력확장을 잘 나타내었으며, 흐름 양상의 계산에는 3가지 경우 모두 유사하게 흐름을 재현함을 보였다.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2001년도 추계 학술대회논문집
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• pp.51-57
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• 2001

The eddy viscosity turbulence models were applied to predict the flows through a cascade, and the prediction performances of turbulence models were assessed by comparing with the experimental results for a controlled diffusion(CD) compressor blade. The original $\kappa-\omega$ turbulence model and $\kappa-\omega$ shear stress transport(SST) turbulence model were used as two-equation turbulence model which were enhanced for a low Reynolds number flow and the Baldwin-Lomax turbulence model was used as algebraic turbulence model. Farve averaged Wavier-Stokes equations in a two-dimensional, curvilinear coordinate system were solved by an implicit, cell-centered finite-volume computer code. The turbulence quantities are obtained by lagging when the men flow equations have been updated. The numerical analysis was made to the flows of CD compressor blade in a cascade at three different incidence angles (40. 43.4. 46 degrees). We found the reversion in the prediction performance of original $\kappa-\omega$ turbulence model and $\kappa-\omega$ SST turbulence model when the incidence angie increased. And the algebraic Baldwin-Lomax turbulence model showed inferiority to two-equation turbulence models.

• 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.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2005년도 춘계 학술대회논문집
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• pp.142-147
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• 2005

A numerical study of 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 temperature. The unsteady Reynolds-averaged Navier-Stokes (URANS) equation method is used together with the SIMPLE algorithm. The results of the present study show that the temporal oscillation of temperature is predicted only by the V2-f model, and the accuracy of the mean velocity, the turbulent shear stress and the mean temperature is a little dependent on the turbulence model used. The the two-layer model and the SST model shows nearly the same capability of predicting the thermal striping and the amplitude of the temperature fluctuation is predicted best by the V2-f model.

• 설비공학논문집
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• 제27권4호
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• pp.220-227
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• 2015

Complex thermal hydraulic characteristics exist inside the reactor because the reactor internals consist of fuel assembly, internal structures and so on. In this study, to examine the effect of Reynolds-Averaged Navier-Stokes (RANS)-based two-equation turbulence models in the analysis of flow distribution inside a 1/5 scaled-down APR+, simulation was performed using the commercial computational fluid dynamics software, ANSYS CFX R.13 and the predicted results were compared with the measured data. It was concluded that reactor internal flow pattern was locally different depending on the turbulence models. In addition, the prediction accuracy of k-${\varepsilon}$ model was superior to that of other two-equation turbulence models and this model predicted the relatively uniform distribution of core inlet flow rate.

• International Journal of Aeronautical and Space Sciences
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• 제13권3호
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• pp.307-316
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• 2012

Numerical simulations of 3D aircraft configurations are performed in order to understand the effects of turbulence models on the prediction of aircraft's aerodynamic characteristics. An in-house CFD code that solves 3D RANS equations and two-equation turbulence model equations are used. The code applies Roe's approximated Riemann solver and an AF-ADI scheme. Van Leer's MUSCL extrapolation with van Albada's limiter is also adopted. Various versions of Menter's $k-{\omega}$ SST turbulence models as well as Coakley's $q-{\omega}$ model are incorporated into the CFD code. Menter's $k-{\omega}$ SST models include the standard model, the 2003 model, the model incorporating the vorticity source term, and the model containing controlled decay. Turbulent flows over a wing are simulated in order to validate the turbulence models contained in the CFD code. The results from these simulations are then compared with computational results from the $3^{rd}$ AIAA CFD Drag Prediction Workshop. Numerical simulations of the DLR-F6 wing-body and wing-body-nacelle-pylon configurations are conducted and compared with computational results of the $2^{nd}$ AIAA CFD Drag Prediction Workshop. Aerodynamic characteristics as well as flow features are scrutinized with respect to the turbulence models. The results obtained from each simulation incorporating Menter's $k-{\omega}$ SST turbulence model variations are compared with one another.

• 한국전산유체공학회지
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• 제2권2호
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• pp.9-17
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• 1997

The performance of several turbulence models in computing an axisymmetric supersonic base flow is investigated. A compressible Navier-Stokes code, which incorporates k-ε, k-ω model and Reynolds stress closure with three kinds of pressure-strain correlation model, has been developed using implicit LU-SGS algorithm with second-order upwind TVD scheme. Numerical computations have been carried out for Herrin and Dutton's base flow. It is observed that the two-equation models give large backward axial velocity approaching to the base and somewhat larger variation of base pressure distribution than the Reynolds stress model. It is also found that the Reynolds stress model with third order pressure-strain model in the anisotropy tensor predicts most accurate mean flow field.

• 한국해양학회지
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• 제30권1호
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• pp.13-26
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• 1995

Blumberg와 Mellor(1987)의 2 방정식 난류모형, Bleackadar(1962)의 1 산정식을 이용한 1 방정식 난류모양 및 Prandtl(1925)의 혼합거리식을 이용한 0 방정식 난류모 양을 일련의 등밀도 문제에 적용 비교하였다. 구체적으로 일정유량이 주어진 수심이 급변하는 수로의 흐름, 유한수로에서 의 조류의 연직구조 및 일정수심 수로에서 의 정 상상태 취송류 문제에 대하여 비교되었다. 불규칙한 수심에 일정유량이 주어진 수로 흐름 및 점모양을 이용한 조류의 수치실험에서는 적용된 난류모양 모두 거의 비슷한 결과를 보였으며, 비교적 관측된 유속구조와 부합하는 좋은 결과를 보였다. 그러나 정 상상태의 취송류 경우에는 2 방정식만이 관측된 유속과 부합하는 유속구조를 재현하 였으며, Blackadar의 l 산정식을 이용한 1, 0 방정식 난류모형은 수면근처의 유속을 관측치보다 작게 계산하였다. 이류항 및 수평확산항의 영향이 작은 조류 및 취송류의 경우, 2 방정식 난류모형에 의한 연직와점성계수 이류항 및 수평확산항의 영향이 작은 조류 및 취송류의 경우, 2 방정식 난류모양에 의한 연직와점성계수 및 특성길이의 연 직분포는 중간수심에서 최대값을 갖는 포물형이었으며, Blackadar의 l 산정식을 사용 한 1, 0 방정식 난류모형에 의한 연직와점성계수 및 혼합특성길이의 연직분포는 수면 에서 최대인 선형에 가까웠다.

• 한국전산유체공학회지
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• 제9권2호
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• pp.30-35
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• 2004

A numerical study of underexpanded jet and impingement on a wall mounted at various distances from the nozzle exit is presented. The 3-dimensional Wavier-Stokes equations and κ-ω turbulence equations are solved. The grids are constructed as overlapped grid systems to examine the distance effect. The DADI method is applied to obtain steady-state solutions. To avoid numerical instability such as the carbuncle phenomena that sometimes accompany approximate Riemann solver, the HLLE+ scheme is employed for the inviscid flux at the cell interfaces. A goal of this work is to apply a number of two-equation turbulence models based on the w equation to the impinging jet problem.

• 한국해안해양공학회지
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• 제6권3호
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• pp.205-215
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• 1994

난류모형을 도입하여 풍성류에 대한 3차원 수치모형을 수립하고, 풍성류 계산에 있어서 연직 와점성계수 산정방법들에 대한 비교평가를 수행하였다. 검토된 방법은 함수형(0-방정식), 1-방정식, 2개의 2-방정식 난류모형($ extsc{k}$-$\varepsilon$과 $textsc{k}$-ι)이며, 난류모형은 난류확산 특성길이의 연직분포에 대한 비교를 통하여 각 방법의 특징이 검토되었다. 양단이 막힌 수로와 순환수로에서 유속의 연직분포 계산결과를 수리실험자료와 비교검증하였다. 분석결과에 의하면 1-방정식 난류모형에 적합한 난류확산 특성길이 산정식은 포물선형이었으며, 2-방정식 난류모형($textsc{k}$-ι 모형과 $textsc{k}$-$\varepsilon$모형)은 대체로 실험치와 일치하는 경향을 보였다. 바람에 의한 영향이 전수심에 미치지 않는 경우에 가정된 연직 와점성계수의 분포는 바람이 영향을 미치는 수심까지만 적용되며, 영향이 없는 수심에서는 연직확산이 거의 일어나지 않아 적정성계수의 크기가 0에 가까웠다.