• Journal of applied mathematics & informatics
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• 제16권1_2호
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• pp.307-321
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• 2004

In this paper, the unsteady Stokes problem is considered and also the pressure-correction method for the problem is described. At a fixed time level, we reduce the problem to two symmetric positive definite problems which depend on a time step parameter. Linear systems that arise from the problems are large, sparse, symmetric, positive definite and ill-conditioned as the time step tends to zero. Preconditioned problems based on an additive Schwarz method for solving the symmetric positive definite problems are derived and preconditioners are defined implicitly. It will be shown that the rate of convergence is independent of the mesh parameters as well as the time step size.

• 한국기계가공학회지
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• 제18권2호
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• pp.73-81
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• 2019

Numerical simulations are performed for the thermal fluid flow around a circular cylinder, and the particle trajectories are calculated to investigate the particle motions and deposition characteristics. We aim to understand the effects of three important parameters (particle Stokes number, temperature difference in the flow and on the cylinder surface, and thermal conductivity ratio between the fluid and the particles) on the deposition efficiency. The results show that the thermophorectic effect is insignificant for particles with large Stokes numbers, but it affects particles with small Stokes numbers. The deposition efficiency increases with the increase in temperature difference between the flow and the cylinder or the decrease in ratio of thermal conductivity of the particles to the fluid. When thermophoresis becomes significant, the particles are deposited even on the back side of the cylinder.

• Journal of the Optical Society of Korea
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• 제14권4호
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• pp.431-437
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• 2010

A stack of gradient-index (GRIN) rod lenses cannot be used for coherent anti-Stokes Raman scattering (CARS) microendoscopy for insertion to internal organs through a surgical keyhole with minimal invasiveness. That's because GRIN lens has large amount of inherent chromatic aberrations in spite of absolutely requiring a common focus for pump and Stokes beam with each frequency of ${\omega}_p$ and ${\omega}_S$. For this endoscopic purpose, we need to develop a long slender probe-type objective, namely probe-type microscope objective (PMO). In this paper, we introduce the structure, the working principle, and the design techniques of PMO which is composed of a probe-type lens module (PLM) and an adaptor lens module (ALM). PLM is first designed for a long slender type and ALM is successively designed by using several design parameters from PLM for eliminating optical discords between scanning unit and PLM. A combined module is optimized again to eliminate some coupling disparities between PLM and ALM for the best PMO. As a result, we can obtain a long slender PMO with perfectly diffraction-limited performance for pump beam of 817 nm and Stokes beam of 1064 nm.

• 한국유체기계학회 논문집
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• 제19권1호
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• pp.37-44
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• 2016

In this study, a parametric study of a centrifugal pump with double volute has been performed numerically using three-dimensional Reynolds-averaged Navier-Stokes equations. The shear stress transport model was selected as turbulence closure through turbulence model test. The finite volume method and unstructured grid system were used for the numerical analysis. The optimal grid system in the computational domain was determined through a grid dependency test. The expansion coefficient, circumferential and radial starting positions and length of divider were selected as the geometric parameters to be tested. And, the hydraulic efficiency and the radial thrust coefficient were considered as performance parameters. It was found that the radial thrust and hydrualic efficiency are more sensitive to the expansion angle and circumferential starting position of the divider than the other geometrical parameters.

• Spatial Information Research
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• 제17권3호
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• pp.397-404
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• 2009

기존의 우리나라 지상중력자료는 자료의 분포 및 정밀도에 있어서 문제점을 가지고 있었고 이러한 문제를 해결하기 위하여 2008년 항공중력측정을 통하여 정밀도 1.56mGal의 항공중력자료를 확보한 바 있다. 그러나 항공중력자료는 비행고도 상에서 획득된 값으로 기존의 지상중력자료 및 해상중력자료와 병합하기 위해서는 지표면 상의 값으로 환산되어야 한다. 또한 다양한 자료를 융합하여 정밀한 지오이드를 계산하기 위해서는 Stokes' 적분반경, Stokes' kernel 및 지형 효과 계산 반경 등의 많은 변수들을 최적으로 고려하여야 한다. 본 연구에서는 지상 및 항공중력자료의 분포 및 특성을 고려하여 보다 정밀한 지오이드 결정을 위한 최적의 매개변수들을 결정하고자 하였다. 선정된 최적 변수들을 적용하여 지오이드를 계산한 결과, 항공중력 및 지상중력 기반의 두 지오이드는 평균 -16.95cm, 표준편차 ${\pm}8.50cm$의 차이를 나타내었는데, 이는 지상 및 항공중력자료의 분포와 지상중력자료에 포함된 오차에 기인한 것으로 판단된다. 향후 본 연구에서 고려한 매개변수 외에도 다양한 하향연속 방법, 지형효과 계산 방법이 지오이드에 미치는 효과와 추가적으로 확보한 중력 및 GPS/Leveling 자료, 해상중력자료를 포함하였을 때의 효과에 대한 연구도 진행되어야 할 것이다.

• 생약학회지
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• 제34권4호통권135호
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• pp.339-343
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• 2003

We investigated the effects of Rhus verniciflua Stokes (RVS) on high fat diet- induced obesity in C57BL/6 that received ad libitum exposure to a high fat diet for 8 weeks. Male C57BL/6 mice weighing $20.1{\pm}0.95\;g$ were divided into four groups and the body weight and food intake were weighed for 8 weeks. After the administration of RVS extract, the liver, subcutaneous and retroperitoneal adipose tissue in the mice were weighed and common blood count in whole blood and biochemical parameters in plasma were measured. It was founded that body weight increase was significantly suppressed by the oral administration of RVS extract in group with high fat diet. Weight of subcutaneous adipose tissue and concentration of triglyceride in plasma from mice which were administrated RVS extract were lower than obesity control group. These results suggest that RVS extract may effect on inhibition of diet-induced obesity.

• 한국추진공학회지
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• 제6권1호
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• pp.71-82
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• 2002

본 연구에서는 2차원의 압축성 Navier-Stokes 코드를 개발하여 mixer-ejector 노즐의 유동장 해석을 다양한 덕트와 노즐 면적비 및 노즐 압력비에 대하여 계산을 수행하였다. 덕트와 노즐 면적비 계산에서는 먼저 효율적인 2차 유동의 유입을 위한 최적의 면적비가 있음을 볼 수 있었다. 높은 면적비에서는 입구 자유유동의 적절한 혼합없이 mixing duct를 그대로 통과하는 것을 볼 수 있었고, 낮은 면적비에서는 제트의 경계가 유입 유동에 장애물로 작용하는 것을 볼 수 있었다. 노즐 압력비의 계산에 있어서는 shroud 벽면과 shock cell structure 간에 상호작용이 작다면 유입유량은 압력비에 따라 증가하는 것을 볼 수 있었다.

• 한국전산유체공학회지
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• 제20권2호
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• pp.37-45
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• 2015

A parametric study on the shapes of bobsleigh bumpers has been performed to reduce the aerodynamic drag. Effects of geometric parameters, such as leading angle of leading bumper, the ratio of minimum width to maximum width of leading bumper, the ratio of leading bumper length to trailing bumper length, trailing angle of trailing bumper, and the ratio of bumper height to installation location of bumper from the bottom of bobsleigh, on the aerodynamic performance of the bobsleigh were estimated using 3-D Reynolds-averaged Navier-Stokes equations. The turbulence was analyzed using the shear stress turbulence model. Reynolds number based on the hydraulic diameter of the external flow channel was in the range of 150,000~1,000,000. Numerical results for drag coefficient were validated compared to experimental data. Ranges of the five geometric parameters were determined according to the rule of Federation Internationale de Bobsleigh et de Tobaganning. The aerodynamic performance of the bobsleigh sled was most sensitive to the leading angle of leading bumper and the ratio of minimum width to maximum width of leading bumper.

• Journal of Advanced Marine Engineering and Technology
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• 제32권2호
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• pp.284-291
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• 2008

This study presents an aerodynamic design and numerical analysis of a centrifugal compressor in gas turbines for SOFC-gas turbine hybrid system application. Total-to-total pressure ratio of the compressor is 3.6:1 that could be used widely for small and large SOFC-gas turbine systems. The compressor consists of a centrifugal impeller and a wedge diffuser. Conceptual design and aerodynamic design with mean line analysis and quasi-3D analysis are performed, and aerodynamic parameters as well as design variables are discussed from the design results. A numerical analysis based on the Reynolds-averaged Navier-Stokes equation was performed for the flow analysis of the compressor. The results show that the centrifugal compressor designed meets the design target, and the aerodynamic parameters and results of the compressor can be used for the aerodynamic design of centrifugal compressors and the feasibility study of SOFC-gas turbine system design.

• 한국유체기계학회 논문집
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• 제15권4호
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• pp.19-26
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• 2012

In this paper, a parametric study on ribs which are installed in an equilateral triangular internal cooling channel is presented. The numerical analysis of the flow structure and heat transfer characteristics is performed using three-dimensional Reynolds-averaged Navier-Stokes equations with the shear stress transport turbulence model. The numerical results are obtained at Reynolds number, 20,000. The parametric study is performed for the parameters, the angle of a rib, rib pitch-to-hydraulic diameter ratio, rib width-to-hydraulic diameter ratio, and rib height-to-hydraulic diameter ratio. The computational results are validated with the experimental data for area-averaged Nusselt number.