• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 1998년도 추계 학술대회논문집
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• pp.55-61
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• 1998

The purpose of this study is to compare the predictive behaviors of the extended $k-{\varepsilon}$ turbulence model and the standard $k-{\varepsilon}$ turbulence model. Grid dependency is tested with the H-type grid and the O-type grid. Computations have been performed for a circular-to-rectangular transition duct. Numerical results for several sections along the streamwise have been obtained to compare with experimental results. The Reynolds number is 390,000 based on the bulk velocity at the inlet. The computed axial velocity contours, transverse velocity profiles, static pressure contours, peripheral skin friction coefficient, and peripheral wall static pressure distributions have been compared with experimental results. The computed results obtained with the extended $k-{\varepsilon}$ turbulence model show better agreement with experimental results than those obtained with the standard $k-{\varepsilon}$ turbulence model. Comparing to the computed results obtained with the H-type grid and O-type grid, those with H-type grid agree well with experimental results.

• 한국추진공학회지
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• 제4권4호
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• pp.9-17
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• 2000

준안정상인 $\beta$형 HNIW의 용해와 안정상인 $\varepsilon$형 HNIW의 성장 특성을 고려한 모델식을 물질수지와 한께 계산하는 방법으로 결정성장 속도와 용해 속도를 계산하였다. 제시된 모델은 용액을 매체로 하여 진행되는 $\beta$$\longrightarrow$$\varepsilon$전이 현상에 대한 속도론적 데이터를 모사 하는데 유용하였다. 2 단 모델을 이용한 유효 인수로부터, 격정성장 과정에서 표면 축적 단계의 영향은 작으며, 확산 의존성은 ethyl acetate와 chloroform의 혼합 용매 중 chloroform의 함량이 증가함에 따라 감소함을 보였다. 이들 속도론 적 계수들을 이용한 수치모사를 통하여 $\varepsilon$-HNIW의 입자 크기를 예측하는 것이 가능하였다.

• 한국항공우주학회지
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• 제31권8호
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• pp.1-7
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• 2003

본 연구에서는 새로운 $\varepsilon$-SST 난류 모델을 이용하여 벽면 근처에 위치한 정사각주 주위의 유동장에 대한 수치해석을 수행하였다. SST 난류 모델을 수정하여 새롭게 제안된 $\varepsilon$-SST 모델은 뭉툭한 물체 주위의 박리 영역에서 기존의 2-방정식 난류 모델보다 향상된 해석 결과를 보임을 확인하였다. $\varepsilon$-SST 모델을 이용하여 박리가 수반되는 유동영역에 대한 효율적인 해석이 가능할 것이다. 또한, 본 연구에서는 임계 간극 이하에서는 주기적인 와류배출이 억제됨을 입증하였으며, 스트로할수는 간극의 높이와 벽면 경계층의 두께의 영향을 받는 다는 것을 확인할 수 있었다.

• Transactions on Electrical and Electronic Materials
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• 제13권4호
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• pp.196-199
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• 2012

CdS thin film was prepared on glass substrate by chemical bath deposition in an alkaline solution. The optical properties of CdS thin film were investigated using spectroscopic ellipsometry. The real (${\varepsilon}_1$) and imaginary (${\varepsilon}_2$) parts of the complex dielectric function ${\varepsilon}(E)={\varepsilon}_1(E)+i{\varepsilon}_2(E)$, the refractive index n(E), and the extinction coefficient k(E) of CdS thin film were obtained from spectroscopic ellipsometry. The normal-incidence reflectivity R(E) and absorption coefficient ${\alpha}(E)$ of CdS thin film were obtained using the refractive index and extinction coefficient. The critical points $E_0$ and $E_1$ of CdS thin film were shown in spectra of the dielectric function and optical constants of refractive index, extinction coefficient, normal-incidence reflectivity, and absorption coefficient. The dispersion of refractive index was analyzed by the Wemple-DiDomenico single-oscillator model.

• 폴리머
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• 제35권4호
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• pp.325-331
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• 2011

침투 가능한 수형 모델 유체의 방정식을 고찰하는 다양한 범위의 입자 충전 분을 ${\phi}$ 및 척력적 에너지 상수 ${\varepsilon}^*$에 대하여 분자 동력학 방법을 이용한 전산 모사를 수행하였다. 전산 모사로부터 얻어진 결과는 문헌에 보고된 고침투 근사식 및 저침투 근사식으로 알려진 두 가지의 한계적 이론식들과 직접 비교하였다. 낮은 척력적 에너지를 갖는 ${\varepsilon}^*$ <3.0의 경우 전산 모사 결과는 이들 두 이론식들과 일치하였으나, 반면 입자간 상호 포텐셜 에너지가 입자 자체 평균 운동 에너지의 두 배 이상 높은 척력적 에너지를 갖는 ${\varepsilon}^*{\geqq}3.0$의 경우 이들 이론식들 모두 전산 모사 결과를 재현하지 못하였다. 이는 특히 높은 입자 밀도와 높은 척력적 에너지를 갖는 ${\phi}{\geqq}0.7$ 및 ${\varepsilon}^*$=6.0의 경우 입자들의 클라스터 형성 및 자체 입자 배제 부피에 따른 비연속적 크기 효과에 기인되었다.

• 한국자동차공학회논문집
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• 제6권5호
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• pp.86-96
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• 1998

A numerical study has been carried out of three-dimensional turbulent flows around a MIRA reference vehicle model both with and without wheels in computation. Two convective difference schemes with two k-$\varepsilon$ turbulence models are evaluated for the performance such as drag coefficient, velocity and pressure fields. Pressure coefficients along the surfaces of the model are compared with experimental data. The drag coefficient, the velocity and pressure fields are found to change considerably with the adopted finite difference schemes. Drag forces computed in the various regions of the model indicate that design change decisions should not rely just on the total drag and that local flow structures are important. The results also indicate that the RNG model with the QUICK scheme predicts fairly well the tendency of velocity and pressure fields and gives more reliable drag coefficient rather than the other cases.

• 대한기계학회논문집B
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• 제27권6호
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• pp.821-827
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• 2003

Fully developed turbulent flow in a square duct is numerically predicted with two nonlinear low-Reynolds-number ${\kappa}-{\varepsilon}$ models. Typical predicted quantities such as axial and secondary velocities, turbulent kinetic energy and Reynolds stresses are compared in detail with each other. It is found that the nonlinear low-Reynolds-number ${\kappa}-{\varepsilon}$ model adopted in a commercial code is unable to predict accurately duct flows involving turbulence-driven secondary motion with the prediction level of secondary flows one order less than that of the experiment.

• Journal of Advanced Marine Engineering and Technology
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• 제23권2호
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• pp.216-225
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• 1999

Four turbulent $k-{varepsilon}$models(i.e standard model modified models with streamline curvature modification and/or preferential dissipation modification) are applied in order to analyze the tur-bulent flow of wall-attaching offset jet. The upwind numerical scheme was adopted in the present analyses. The streamline curvature modification results in slightly better prediction while the preferential dissipation modification does not. The obtained analytic results will be used as refer-ences for further study regarding Reynolds stress model. In addition this paper introduced a method of increasing nozzle outlet velocity gradually for numercal convergence. Even though the method was simple it was efficient in view of convergent speed CPU running time computer memory storage programming etc.

• 대한토목학회논문집
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• 제34권3호
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• pp.813-820
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• 2014

본 연구에서는 부분 식생된 개수로에서 평균흐름 및 난류구조에 관한 수치모의 결과를 제시하였다. 이를 위하여 식생항력항이 포함된 레이놀즈 평균 Navier-Stokes 방정식을 수치해석 하였고 난류 모형으로 비선형 k-${\varepsilon}$ 모형을 이용하였다. 제시된 모형을 Nezu and Onitsuka (2001)의 실험수로에 적용하여 모의된 결과를 실험 계측자료 및 Kang and Choi (2006)의 Reynolds stress model 모의결과와 비교하였다. 실험결과와 비교한 결과에 따르면, 비선형 k-${\varepsilon}$ 모형이 평균흐름의 대체적인 경향을 잘 모의하는 것으로 확인되었다. 또한, 식생 영역과 비식생 영역의 경계면에서 쌍와 (twin vortices)가 생성되고 난류강도와 레이놀즈 응력의 최대점이 위치하는 것을 확인하였다. 레이놀즈 응력에 대해서는 경향은 잘 모의하지만 정량적으로 과소 산정하는 것으로 나타났다.

• 대한기계학회논문집B
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• 제24권2호
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• pp.204-213
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• 2000

This study deals with jet impingement, which is extensively used in the process industries to achieve intense heating, cooling or drying rates and also widely employed as a test flow for turbulent models due to its complex flow configuration, on a flat plate by numerical methods. In this calculation, the finite volume method was employed to solve the Navier-stokes equation based on the non-orthogonal coordinate with non-staggered variable arrangement. To get a better understanding for the fluid flow and heat transfer characteristics of the turbulent jet impingements, $k-{\varepsilon}-{\overline{v^{'2}}}$ turbulent model was adapted and compared with the experimental data and the result of standard $k-{\varepsilon}$ turbulent model. Numerical calculations were carried out with various flow rates, nozzle to plate distances. In the case of the axisymmetric jet impingement on a flat plate, $k-{\varepsilon}-{\overline{v^{'2}}}$ turbulent model showed better agreement with the experimental data than the standard $k-{\varepsilon}$ turbulent model in the prediction of the mean velocity profiles, the turbulent velocity profiles. the turbulent shear stress and the heat transfer rate. The highest heat transfer rate can be obtained when the impingement occurs within the potential core..