• 한국전산유체공학회:학술대회논문집
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• 2000.10a
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• pp.135-140
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• 2000

Numerical calculations are carried out in order to evaluate the performance of low-Re Reynolds stress model based on SSG model for a swirling turbulent flow in a pipe. The results are compared with those of $\kappa-\epsilon$ model and GL model, and the experimental data. The finite volume method is used for the discretization, and the power-law scheme is employed as a numerical scheme. The SIMPLE algorithm is used for velocity-Pressure correction in the governing equations.

• Proceedings of the Korea Water Resources Association Conference
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• 2006.05a
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• pp.594-597
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• 2006

조.세립상(組.細粒床) 대상(帶狀)연속구조를 갖는 개수로 흐름의 부유사 농도분포를 수치모의 하였다. 흐름의 지배방정식인 Navier-Stokes 방정식은 레이놀즈응력모형을 이용하여 해석되었으며, 와점성계수 개념을 이용하여 부유사 수송 방정식을 해석하였다. 기존의 실험결과와 비교하여 모형의 검증을 실시하였으며, 동일한 흐름에 대하여 부유사 농도 분포를 계산하였다. 부유사량의 계산 결과 매끈한 하상 위의 노도분포가 거친하상 위 보다 크게 나타났다. 또한 수치모의로부터 산정된 와확산계수를 Wang and Cheng(2005)이 제안한 해석적 방법과 비교 하였다.

• Journal of computational fluids engineering
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• v.2 no.2
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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.

• Transactions of the Korean Society of Mechanical Engineers
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• v.17 no.2
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• pp.416-425
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• 1993

To investigate the characteristics of the merged jet arising from the interaction of two opposing curved wall jets over a circular cylinder in still air, mean velocity, Reynolds stresses, triple moments and integral length scale were measured using hot-wire anenometry. The turbulent kinetic energy and shear stress budget were evaluated using the measured data. The variations of the Reynolds stresses, the triple moment and integral length scale are severe in the interaction region. The pressure diffusion terms are found to be very large when compared the other terms in the interaction region. The distributions of the Reynolds stress and the triple moment in the similar region are found to be similar to those of conventional plane jets.

• Proceedings of the KSME Conference
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• 2000.11b
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• pp.579-584
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• 2000

Algebraic Reynolds Stress (ARS) model is applied in order to analyze the turbulent flow of wall-attaching offset jet and to evaluate the model's predictability. The applied numerical schemes are upwind scheme and skew-upwind scheme. The numerical results show good prediction in first order calculations (i.e., reattachment length, mean velocity, pressure), while they show slight deviations in second order (i.e., kinetic energy and turbulence intensity). By comparison with the previous results using $k-{\varepsilon}$ model, ARS model predicts better than the standard $k-{\varepsilon}$ model, however, predicts slightly worse than the $k-{\varepsilon}$ model including the streamline curvature modification. Additionally this study can reconfirm that skew-upwind scheme has approximately 25% improved predictability than upwind scheme.

• Transactions of the Korean Society of Mechanical Engineers B
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• v.24 no.12
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• pp.1615-1624
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• 2000

Algebraic Reynolds Stree (ARS) model is applied in order to analyze the turbulent flow of wall-attaching offset jet and to evaluate the predictability of model. The applied numerical schemes are the upwind scheme and the skew-upwind scheme. The numerical results show a good prediction in the first order calculations(i.e., reattachment length, mean velocity, pressure), however, slight deviations in the second order(i.e., kinetic energy and turbulence intensity). Comparing with the previous results using the k-$\varepsilon$ model, the ARS model predicts better than the standard k-$\varepsilon$ model, however, slightly worse than the k-$\varepsilon$ model including the streamline curvature modification. Additionallay this study can reconfirm that the skew-upwind scheme has approximately 25% improved predictability than the upwind scheme.

• Proceedings of the Korea Water Resources Association Conference
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• 2011.05a
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• pp.241-241
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• 2011

일반적으로 식생흐름의 층 적분 모형은 층의 수에 따라 2층 및 3층 모형으로 구분한다. 즉, 전체 수심을 식생영역과 상부영역으로 구분하는 2층 모형과 식생영역을 바닥 조도의 영향 유무에 따라 내부 및 외부 식생영역으로 구분하는 3층 모형으로 나뉜다. 본 연구에 사용된 수리실험 자료는 기존의 연세대학교에서 수행한 실험결과를 이용하여 각 모형의 정확성을 예측해 보았다. 다양한 실험조건에 적용한 결과, 3층 모형이 식생영역에서 유속의 변화를 고려할 수 있지만 레이놀즈응력의 영향에 민감하고, 적분된 유속은 2층 모형에 의한 예측 결과가 더욱 정확하였다. 3층 모형에서는 내부 식생영역의 결과는 전체흐름구조에 미미한 영향을 미치므로 무시할 수 있으며, 이를 바탕으로 식생영역에서 유속 변화가 고려되는 수정 2층 모형을 제시하였다. 본 연구를 통하여 기존의 2층 모형과 3층 모형의 장점을 취합하여 수정된 2층 모형의 방정식을 바탕으로 모형의 정확성을 평가하기 위하여 2층 모형, 3층 모형, 수정 2층 모형의 유속 분포를 비교 분석하여 모형을 검증하였다.

• Proceedings of the Korea Water Resources Association Conference
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• 2007.05a
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• pp.930-934
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• 2007

본 논문은 수리실험을 통해 침수식생 개수로의 단면특성을 살펴보고자 하는 실험논문이다. 레이저 도플러 유속계를 이용하여 측벽으로부터의 거리에 따른 침수식생 개수로의 2차원 순간속도를 측정하였다. 측정된 유속자료를 이용하여, 평균유속, 레이놀즈응력, 난류강도를 살펴보았으며, 침수식생 개수로 흐름의 단면특성을 살펴보았다. 실험결과 침수식생 개수로는 기존의 일반적인 개수로흐름과는 다른 단면 흐름특성을 보이는 것을 확인하였다. 특히 최대유속 발생지점이 수로 중앙이 아닌 측벽 근처로 이동하였으며, 이차흐름의 영향으로 인하여 흐름방향 등유속선의 물결형태와 레이놀즈응력 및 난류강도의 최대값 발생위치 이동과 같은 현상이 발생하는 것을 확인하였다.

• Transactions of the Korean Society of Mechanical Engineers
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• v.19 no.11
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• pp.3014-3021
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• 1995

This study is carried out in order to evaluate the performances of the Reynolds stress turbulence models such as SSG and GL models in the calculation of separated flow over backward-facing stepp.In addition, two slow return-to-isotropy models, YA and Rotta models combined with rapid part of SSG model are also tested. The finite volume method is used to discretize the governing differential equations, and the power-law scheme is used to approximate the convection terms. The SIMPLE algorithm is used for pressure correction in the governing equations. The results show that SSG model gives the better prediction near the reattachment point than GL model. In cases that the rapid term of SSG model is combined with Rotta and YA slow models, the results show the better predictions of stress components in recirculation zone, but indicate inaccuracy in the predictions of mean velocity.

• 유체기계공업학회:학술대회논문집
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• 2003.12a
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• pp.496-501
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• 2003

Reynolds averaged Wavier-Stokes simulations based on the Reynolds stress model was performed to investigated the effect of inlet flow angle on the distributions of the Reynolds stress tensor inside tip leakage vortex of a linear compressor cascade. Two different inlet flow angles ${\beta}=29.3^{\circ}$(design condition) and $36.5^{\circ}$(off-design condition) were considered. Stress tensor analysis, which transforms the Reynolds stress into the principal direction, was applied to show an anisotropy of the normal stresses. Whereas the anisotropy was highest in the region where the tip leakage vortex collides the suction side of the blade and tip leakage flow enters between blade tip of the pressure side and the endwall, it had the lowest value at the center of tip leakage vortex. It was also found that the magnitude of maximum shear stress at design condition was greater than that of off-design condition.