• 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.

• 한국진공학회지
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• 제9권3호
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• pp.242-248
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• 2000

고주파 스퍼터링 방법으로 증착조건을 변화시키면서 BST 박막을 제작하였다. 증착온도가 높을수록, Ar/O$_2$비가 적을수록 우수한 전기적 특성을 보였다. 누설전류 전도기구를 분석하기 위해 Schottky모델과 modified-Schottky모델을 도입하였다. BST 박막의 누설전류 전도기구는 기존의 Schottky모델이 아니라 modified-Schottky 모델을 따른다는 것을 알았다. Modified-Schottky 모델을 사용하여 광학유전상수 $\varepsilon$=4.9, 이동도 $\mu$=0.019 $\textrm{cm}^2$/V-s, 그리고 장벽높이 $\phi_b$ =0.79 eV를 구하였다.

• Journal of the Optical Society of Korea
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• 제18권4호
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• pp.359-364
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• 2014

We report parameters that allow the dielectric functions ${\varepsilon}={\varepsilon}_1+i{\varepsilon}_2$ of $AlAs_xSb_{1-x}$ alloys to be calculated analytically over the entire composition range $0{\leq}x{\leq}1$ in the spectral energy range from 0.74 to 6.0 eV by using the dielectric function parametric model (DFPM). The ${\varepsilon}$ spectra were obtained previously by spectroscopic ellipsometry for x = 0, 0.119, 0.288, 0.681, 0.829, and 1. The ${\varepsilon}$ data are successfully reconstructed and parameterized by six polynomials in excellent agreement with the data. We can determine ${\varepsilon}$ as a continuous function of As composition and energy over the ranges given above, and ${\varepsilon}$ can be converted to complex refractive indices using a simple relationship. We expect these results to be useful for the design of optoelectronic devices and also for in situ monitoring of AlAsSb film growth.

• Journal of Ship and Ocean Technology
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• 제5권2호
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• pp.27-48
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• 2001

Turbulent flow calculations are performed for the two modern practical VLCCs with the sable forebody and the slightly different afterbody, i.e. KVLCC and KVLCC2. Three $\textsc{k}-\varepsilon$ turbulence models are tested to investigate the differences caused by the turbulence models. The calculated results around the two VLCC hull forms using O-O grid topology and profile-fitted surface meshes are compared to the measured data from towing tank experiment. The realizable $\textsc{k}-\varepsilon$model provided realistic wake distribution with hook-like shape, while the standard and RNG-based $\textsc{k}-\varepsilon$models failed. It is very encouraging to see that the CFD with relatively simple turbulence closure can tell the difference quantitatively as well as qualitatively for the two hull forms with stern frameline modification.

• 대한토목학회논문집
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• 제28권6B호
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• pp.643-651
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• 2008

본 연구에서는 횡방향 언덕-저면의 하상형상을 갖는 개수로 흐름을 수치모의 하였다. 곡선좌표계에 대한 지배방정식을 유도하고, 난류폐합을 위해 Speziale(1987)가 제안한 비선형 $k-{\varepsilon}$ 모형을 이용하였다. 개발된 모형의 개수로 흐름에 대한 적용성 및 모형 상수의 민감도를 분석하기 위해 직사각형 개수로 흐름을 수치모의 하였다. 그 결과 모형상수 $C_D$와 $C_E$는 각각 이차흐름 강도 및 난류의 비등방성에 영향을 미치는 것으로 확인되었다. 또한 비선형 $k-{\varepsilon}$ 모형이 자유수면에서 발생되는 난류의 비등방성을 정확히 모의할 수 없는 것으로 나타났으나, 전반적인 이차흐름 분포는 비교적 잘 예측하는 것으로 확인되었다. 한편 개발된 모형을 이용하여 횡방향 하상형상을 갖는 개수로 흐름을 수치모의하고 기존의 실험 결과와 비교하였다. 그 결과 비선형 $k-{\varepsilon}$ 모형이 하상형상의 언덕과 저면에서 발생되는 상향류 및 하향류를 비교적 정확히 예측하는 것으로 나타났으며, 계산된 주흐름방향 평균유속 및 난류구조 역시 기존의 실험 결과와 잘 일치하였다. 그러나 비선형 $k-{\varepsilon}$ 모형은 하상형상의 저면을 향하는 하향류를 과소 산정하는 것으로 확인되었다.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2000년도 춘계학술대회논문집B
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• pp.479-484
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• 2000

A Navier-stokes based finite volume method has been developed to analyze an incompressible, steady state, turbulent wall-jet flow. The standard k-e model, the RNG ${\kappa}-{\varepsilon}$ model and their nonlinear counterparts are adopted as a closure relationship. Comparison with the experimental data shows that a linear ${\kappa}-{\varepsilon}$ model performs satisfatorily for two-dimensional wall-jet flows. However, as the flow becomes three dimensional, the linear model fails to predict the spanwise jet growth accurately and the nonlinear model needs to be adopted to capture three-dimensional flow characteristics.

• 한국도로학회논문집
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• 제12권4호
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• pp.147-155
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• 2010

재활용된 암버력-토사의 회복탄성계수 예측모델이 개발되었다. 반복삼축시험을 통한 회복탄성계수의 전통적 평가방법은 큰 입경을 가진 자갈에는 실현 불가능하다. 미세한 차이가 있는 비선형 전단탄성계수를 이용하여 회복탄성계수를 산출하는 대체기법을 제안하였다. 현장에서 측정한 최대전단탄성계수와 대형공진주 시험으로 구한 감소곡선을 이용하여 회복탄성계수 예측모델을 개발하였다. 이 예측모델을 김천의 고속도로공사현장에서 재활용한 암버력-토사에 적용하여 모델인자 $A_E,\;n_E,\;{\varepsilon}_r,\;{\alpha}$를 각각 9618, 0.47, 0.0135, 0.8로 제안하였다.

• 대한기계학회논문집B
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• 제25권3호
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• pp.305-314
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• 2001

A modified model is proposed for calculation of transitional boundary layer flows. In order to develop the eddy viscosity model for the problem, the flow is divided into three regions; namely, pre-transition region, transition region and fully turbulent region. The pre-transition eddy-viscosity is formulated by extending the mixing length concept. In the transition region, the eddy-viscosity model employs two length scales, i.e., pre-transition length scale and turbulent length scale pertaining to the regions upstream and the downstream, respectively, and a universal model of stream-wise intermittency variation is used as a function bridging the pre-transition region and the fully turbulent region. The proposed model is applied to calculate three benchmark cases of the transitional boundary layer flows with different free-stream turbulent intensity (1%∼6%) under zero-pressure gradient. It was found that the profiles of mean velocity and turbulent intensity, local maximum of velocity fluctuations, their locations as well as the stream-wise variation of integral properties such as skin friction, shape factor and maximum velocity fluctuations are very satisfactorily predicted throughout the flow regions.

• Wind and Structures
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• 제23권5호
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• pp.465-483
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• 2016

This study aims to enhance the understanding of the surface pressure distribution around rectangular bodies, by considering aspects such as the suction pressure at the leading edge on the top and side faces when the body aspect ratio and wind direction are changed. We carried out wind tunnel measurements and numerical simulations of flow around a series of rectangular bodies (a cube and two rectangular bodies) that were placed in a deep turbulent boundary layer. Based on a modern numerical platform, the Navier-Stokes equations with the typical two-equation model (i.e., the standard $k-{\varepsilon}$ model) were solved, and the results were compared with the wind tunnel measurement data. Regarding the turbulence model, the results of the $k-{\varepsilon}$ model are in overall agreement with the experimental results, including the existing data. However, because of the blockage effects in the computational domain, the pressure recovery region is underpredicted compared to the experimental data. In addition, the $k-{\varepsilon}$ model sometimes will fail to capture the exact flow features. The primary emphasis in this study is on the flow characteristics around rectangular bodies with various aspect ratios and approaching wind directions. The aspect ratio and wind direction influence the type of wake that is generated and ultimately the structural loading and pressure, and in particular, the structural excitation. The results show that the surface pressure variation is highly dependent upon the approaching wind direction, especially on the top and side faces of the cube. In addition, the transverse width has a substantial effect on the variations in surface pressure around the bodies, while the longitudinal length has less influence compared to the transverse width.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2003년도 The Fifth Asian Computational Fluid Dynamics Conference
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• pp.13-14
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• 2003

Two different ${\kappa}-{\varepsilon}-\overline{{\nu}{\nu}}-f$ turbulence models together with the two-layer model are evaluated for natural convection in a rectangular cavity. The numerical problem and accuracy of the turbulence models are discussed. The original $\overline{{\nu}{\nu}}-f$ model suffers from the numerical stiffness problem when used with the segregate solution procedure like the SIMPLE algorithm, and a remedy for this problem is proposed. It is shown that original $\overline{{\nu}{\nu}}-f$ model best predicts the mean velocity, Reynolds stresses and the turbulent heat flux while the modified $\overline{{\nu}{\nu}}-f$ model (N=6) overpredicts the turbulent quantities.