• 대한조선학회논문집
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• 제55권6호
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• pp.474-481
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• 2018

This paper is to compare by numerical analysis the flow characteristics and propulsion performance of stern with the shape change of K-duct, a pre-swirl duct developed by Korea Research Institute of Ships & Ocean Engineering (KRISO). First, the characteristics of the propeller and the resistance and self-propulsion before and after the attachment of the K-duct to the ship were verified and the validity of the calculation method was confirmed by comparing this result with the model test results. After that, resistance and self-propulsion calculations were performed by the same numerical method when the K-duct was changed into five different shapes. The efficiency of the other five cases was compared using the delivery horsepower in the model scale and the flow characteristics of the stern were analyzed as the velocity and pressure distributions in the area between the duct end and the propeller plane. For the computation, STAR-CCM +, a general-purpose flow analysis program, was used and the Reynolds Averaged Navier-Stokes (RANS) equations were applied. Rigid Body Motion (RBM) method was used for the propeller rotating motion and SST $k-{\omega}$ turbulence model was applied for the turbulence model. As a result, the tangential velocity of the propeller inflow changed according to the position angle change of the stator, and the pressure of the propeller hub and the cap changes. This regulated the propeller hub vortex. It was confirmed that the vortex of the portion where the fixed blade and the duct meet was reduced by blunt change.

• Tribology and Lubricants
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• 제38권5호
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• pp.191-198
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• 2022

With the world's fast expanding energy usage comes a slew of new issues. Because one-third of energy is lost in overcoming friction, tremendous effort is being directed into minimizing friction. Surface texturing is the latest surface treatment technology that uses grooves and dimples on the friction surface of the machine to significantly reduce friction and improve wear resistance. Despite the fact that many studies on this issue have been conducted, most of them focused on parallel surfaces, with relatively few cases of converging films, as in most sliding bearings. This study investigated the lubrication performance of surface-textured inclined slider bearings. We analyzed the continuity and Navier-Stokes equations using a commercial computational fluid dynamics code, FLUENT. The results show the pressure and velocity distributions and the lubrication performance according to the number and orientation of rectangular dimples. Partial texturing somewhat improves the lubrication performance of inclined slider bearings. The number of dimples with the maximum load-carrying capacity (LCC) and minimum friction is determined. When the major axis of the dimple is arranged in the sliding direction, the LCC and friction reduction are maximized. However, full texturing significantly reduces the LCC of the slider bearing and increases the flow rate. The results have the potential to improve the lubrication performance of various sliding bearings, but further research is required.

• Tribology and Lubricants
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• 제39권3호
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• pp.87-93
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• 2023

Nanofluids are dispersions of particles smaller than 100 nm (nanoparticles) in base fluids. They exhibit high thermal conductivity and are mainly applied in cooling applications. Nanolubricants use nanoparticles in base oils as lubricant additives, and have recently started gathering increased attention owing to their potential to improve the tribological and thermal performances of various machinery. Nanolubricants reduce friction and wear, mainly by the action of nanoparticles; however, only a few studies have considered the rheological properties of lubricants. In this study, we adopt a parallel slider bearing model that does not generate geometrical wedge effects, and conduct thermohydrodynamic (THD) analyses to evaluate the effect of higher thermal conductivity and viscosity, which are the main rheological properties of nanolubricants, on the lubrication performances. We use a commercial computational fluid dynamics code, FLUENT, to numerically analyze the continuity, Navier-Stokes, energy equations with temperature-viscosity-density relations, and thermal conductivity and viscosity models of the nanolubricant. The results show the temperature and pressure distributions, load-carrying capacity (LCC), and friction force for three film-temperature boundary conditions (FTBCs). The effects of the higher thermal conductivity and viscosity of the nanolubricant on the LCC and friction force differ significantly, according to the FTBC. The thermal conductivity increases with temperature, improving the cooling performance, reducing LCC, and slightly increasing the friction. The increase in viscosity increases both the LCC and friction. The analysis method in this study can be applied to develop nanolubricants that can improve the tribological and cooling performances of various equipment; however, additional research is required on this topic.

• 해양환경안전학회지
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• 제26권7호
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• pp.931-941
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• 2020

해양데이터를 수집하기 위해 필요한 엔지니어, 연구원 및 과학자를 대신할 수 있는 해양 모니터링 장치인 자율주행보트의 필요성이 대두되고 있다. 이 논문은 자율주행보트의 세일을 개발하기 위한 연구로 곡선형 트윈 세일의 공기역학적인 특성을 수치해석적으로 분석하고 이를 날개 형태의 세일과 성능비교를 통해 곡선형 트윈 세일의 공기 역학적인 성능을 확인하였고, 세일의 간격과 형상에 따른 성능을 비교하였다. 유체 해석을 위한 지배방정식은 Navier - Stokes를 사용하였다. 성능비교 결과 곡선 형 트윈 세일은 날개 형태의 세일과 비교하여 양력, 항력 및 추력 계수가 향상됨을 알 수 있다. 또한, 트윈 세일의 양 날개의 간격은 중요한 변수임을 확인 하였다. 0.035 L, 0.07 L, 0.14 L에서는 스톨로 인해 양력 계수의 감소로 나타났고 0.21 L, 0.28 L, 0.35 L에서는 개선되어 0.28 L에서 최대 양력을 보여준다.

• 한국해안·해양공학회논문집
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• 제22권6호
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• pp.374-386
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• 2010

최근 슬리트케이슨제와 같은 유공방파제의 파랑제어특성에 대한 이론적 실험적 연구가 활발히 진행되고 있다. 본 연구에서는 규칙파의 작용하에 슬리트케이슨에 의한 반사율의 특성과, 전면유공부 및 유수실의 내부벽면에 작용하는 파압을 2차원 및 3차원수치파동수로에서 각각 추정하고, 그 결과를 검토하였다. 수치실험에서는 주기 7초, 9초, 11초 및 13초와 각각의 주기에 대해 파형경사 0.02, 0.03 및 0.04를 갖는 입사파고의 수치실험안을 설정하였고, 본 연구에서 사용된 2차원 및 3차원의 수치해석은 Navier-Stokes운동방정식에 기초한 이상류(이상류(二相流)) 수치 모델로서, 이는 타해석기법에 비해 복잡한 수면변동에 대한 물리현상을 쉽게 재현할 수 있으며, 수치프로그램의 구성이 보다 간략하게 되는 장점이 있다. 실험결과에 의하면, 반사율에 있어서 주기가 짧은 경우에는 2차원해석이 상당히 큰 값을 나타내지만, 주기가 길어지고 파형경사가 큰 경우에는 2차원해석과 3차원해석의 결과가 거의 동일한 값을 나타낸다. 파압에 있어서 주기가 짧은 경우에는 두 해석법에서 차이는 작지만, 주기가 길어지고 파형경사가 큰 경우에는 차이가 크게 나타나는 경향을 확인할 수 있었다.

• 한국전산유체공학회지
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• 제13권4호
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• pp.1-7
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• 2008

In the process of continuous hot-dip galvanizing, it is well known that the gas wiping through an air knife system is most effective because of its uniformity in coating thickness, possibility of thin coating, workability in high speed, and simplicity of control. However, gas wiping used in the galvanizing process brings about a problem of splashing at the strip edge above a certain high speed of process. It is also known that the problem of edge splashing is more harmful than that at the mid strip surface. For a given liquid(of a certain viscosity and surface tension), the onset of splashing mainly depends upon the strip velocity, the gas-jet pressure, and the nozzle's stand-off distance. In these connections in the present study, we proposed three kinds of air knife system having nozzles of constant expansion rate, and compared the jet structures issuing from newly proposed nozzle systems with the result by a conventional one. In numerical analysis, the governing equations are consisted of two-dimensional time dependent Navier-Stokes equations, and the standard k-${\varepsilon}$ turbulence model is employed to solve turbulence stress and so on. As the result, it is found that we had better use the constant expansion-rate nozzle which can be interpreted from the point view of the energy saving for the same coating thickness. Also, we better reduce the size of separation bubble and enhance the cutting ability at the strip surface, by using an air-knife having constant expansion-rate nozzle.

• 한국컴퓨터그래픽스학회논문지
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• 제14권3호
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• pp.19-30
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• 2008

유체 시뮬레이션은 영화나 게임에 등장하는 물, 연기, 불, 폭발, 모래 등과 관련된 애니메이션을 생성하기 위해 유체운동 방정식을 풀어 형상화하는 컴퓨터 그래픽스 기술이다. 본 리뷰 논문은 유체 시뮬레이션에 대한 최근의 연구 동향을 영화를 중심으로 분석한다. 이를 위해 먼저 컴퓨터 그래픽스 분야에서 유체 시뮬레이션을 하는 방법과 이와 관련된 효율적 속도, 사실적 형상화 등의 기술적 이슈들을 격자 방법과 입자방법으로 분류하여 설명한다. 다음으로 2008년 Sci-Tech 오스카상을 수상한 유체 시뮬레이션 연구자 및 개발자들의 업적을 중심으로 그들이 제작한 영화 속에 사용된 기술의 특징을 설명한다. 이 과정을 통해 향후 영상 콘텐츠 분야의 유체 시뮬레이션 연구개발의 발전방향을 짚어보면 유체와 변형체나 고체사이의 상호작용, 상변이에 의한 위상 변화 표현, 유체 기반 크리쳐 생성과 크리쳐와 유체 상호작용 표현 기술이 주목을 받을 것으로 예상한다.

• 대한토목학회논문집
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• 제32권6C호
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• pp.267-274
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• 2012

오염물질의 거동은 간극 배열과 연결망에 의해 결정되지만 흙에서 오염물질의 이동을 계산하는 전통적인 접근은 거시 스케일에서 적용된다. 나비에-스토크스 방정식을 풀기 위해 소요되는 컴퓨팅 비용 때문에 간극 스케일에서 이동과 결과를 관찰하기 쉽지 않다. 본 논문에서는 단일상 다성분 유체유동에서 국부적인 유속과 밀도를 효과적으로 평가할 수 있는 격자 볼츠만 방법에 대해 설명한다. 오염물질의 시공간적 거동은 유체 유동의 이송에 의해 명시적으로 결정된다. 두 가지 형태의 이상화된 간극은 유체의 경로를 제공한다. 또한 오염물질 이동, 유속장, 오염물질의 평균 농도는 정상상태의 유동에서 계산된다. 굴곡비와 같은 간극 형상은 오염물질 거동의 영향을 준다. 이는 흙이나 암반의 불연속면에서 동일한 간극률를 가져도 간극의 배열과 형상의 중요함을 강조한다.

• 한국수소및신에너지학회논문집
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• 제31권4호
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• pp.387-394
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• 2020

A parametric study of a 2.5 kW class propeller type micro hydraulic turbine was performed. In order to analyze the internal flow characteristics in the hydraulic turbine, three dimensional Reynolds-averaged Navier-Stokes equations with shear stress transport turbulence model were used and the hexahedral grid system was used to construct computational domain. To secure the reliability of the numerical analysis, the grid dependency test was performed using the grid convergence index method based on the Richardson extrapolation, and the grid dependency was removed when about 1.7 million nodes were used. For the parametric study, the axial distance at shroud span (L) between the inlet guide vane and the runner, and the inlet and outlet blade angles (β₁, β₂) of the runner were selected as the geometric parameters. The inlet and outlet angles of the runner were defined in the 3 spans from the hub to tip, and a total of 7 geometric parameters were investigated. It was confirmed that the outlet angles of the runner had the most sensitive effect on the power and efficiency of the micro hydraulic turbine.

• 한국전산유체공학회지
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• 제21권2호
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• pp.112-119
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• 2016

NEXTSat-1 is the next-generation small-size artificial satellite system planed by the Satellite Technology Research Center(SatTReC) in Korea Advanced Institute of Science and Technology(KAIST). For the control of attitude and transition of the orbit, the system has adopted a RHM(Resisto-jet Head Module), which has a very simple geometry with a reasonable efficiency. An axisymmetric model is devised with two coil-resistance heaters using xenon(Xe) gas, and the minimum required specific impulse is 60 seconds under the thrust more than 30 milli-Newton. To design the module, seven basic parameters should be decided: the nozzle shape, the power distribution of heater, the pressure drop of filter, the diameter of nozzle throat, the slant length and the angle of nozzle, and the size of reservoir, etc. After quasi one-dimensional analysis, a theoretical value of specific impulse is calculated, and the optima of parameters are found out from the baseline with a series of multi-physical numerical simulations based on the compressible Navier-Stokes equations for gas and the heat conduction energy equation for solid. A commercial code, COMSOL Multiphysics is used for the computation with a FEM (finite element method) based numerical scheme. The final values of design parameters indicate 5.8% better performance than those of baseline design after the verification with all the tuned parameters. The present method should be effective to reduce the time cost of trial and error in the development of RHM, the thruster of NEXTSat-1.