• Proceeding of EDISON Challenge
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• 2016.11a
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• pp.55-57
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• 2016

본 연구에서는 초고속 자기부상열차의 단면도를 통하여 2-D형상을 모델링하고 이를 기반으로 항력과 유동 특성에 대한 분석을 수행하였다. 유동의 마하수가 0.3 이상임을 고려하여 압축성 모델이 사용되었고, 난류모델은 Menter's k-w SST(Shear Stress Transport)모델을 적용시켰다. 2-D 해석과 자기부상열차의 특성상 열차가 공기중에서 주행하고 있는 것으로 가정하고 공력 특성을 해석하였다.

• Journal of the Korean Society for Marine Environment & Energy
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• v.7 no.2
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• pp.82-88
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• 2004

To evaluate the tidal flow around the transmission type harbour structures, the numerical models considering hydraulic resistance are used. The traditional governing equations of depth-integratef hydrodynamics are modified by using of the drag force term. As a numerical model to evaluate the rate of tidal exchange, the Random-walk method is used. The models are applied in a design of the pile-supported pier structures in Busan harbour site, Korea, where the flow speed and the tidal exchange are more promotive than the case of non-transmission structure. The developed model will be applied usefully to design the transmission type structure in the ocean space.

• Journal of the Korea Convergence Society
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• v.10 no.8
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• pp.159-164
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• 2019

The front bumper of bobsleigh is mounted to alleviate the impact, but the air resistance to the bobsleigh depends on the body shape positioned in front. This study was conducted the flow analyses about three kinds of bobsleigh configurations. Models B and C with the sharp type of the front can reduce the air resistance than model A with the round type of the front. And the type that the back of the bumper narrows can generate a flow smoother than the one widening. It is thought that the results of this study can be devoted at ensuring the body design to reduce the flow resistance most at bobsleigh. As the design data with the durability of bobsleigh obtained on the basis of this study result are utilized, the esthetic sense can be shown by being grafted onto the machine or structure at real life.

• Proceedings of the KAIS Fall Conference
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• 2011.12b
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• pp.525-528
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• 2011

1400cc급 발전용 엔진 트로틀 바디의 최적화 및 성능 향상을 위하여 유동해석을 수행하였다. 베르누이 정리를 기본으로, 성능을 발휘하는 주요 설계인자인 트로틀 바디 내부의 트로틀 밸브 각도 및 흡기부 곡률 등을 설계 변수로 유동해석을 수행하였다. 벤튜리관 흡입부의 곡률을 증가시켜 트로틀 바디에서 소모되는 흡기저항을 줄였다. 감소된 흡기저항은 펌핑로스를 저감하여 연비향상에 도움이 될 것으로 기대된다. 결과적으로 해석결과 분석을 통하여 최적화된 모델을 제시하였다.

• Proceeding of EDISON Challenge
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• 2012.04a
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• pp.37-40
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• 2012

EDISON CFD 수치 해법 기법을 바탕으로 초음속 유동장 속에서 spike가 부착된 무딘 물체에 대하여, spike 형상 변화에 따른 압축성 효과에 의한 항력 변화 추이를 고찰하였다. Spike의 길이 따른 항력 변화 추이를 살펴보았다. Spike의 길이가 Main body와 특정한 비율을 가질 때 항력이 최소가 된다. 이를 기준으로 spike 길이가 특정 길이만큼 줄어들거나 늘어날 경우에 각각 1.35%, 4.95% 항력이 증가하였다. 이러한 자료들은 초음속 유동장에서 무딘 물체에 가해지는 압축성 효과에 의한 저항을 최소화하기 위한 spike 설계 시 중요한 견해를 제공한다.

• Journal of the Korean Society of Mechanical Technology
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• v.13 no.1
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• pp.41-47
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• 2011

In this study, the structural analysis of cooling fan is combined with 3-D flow analysis by using CFD on fluid domain. The smoothly cooling flow with optimum design of cooling parts is essential at automotive combustion engine. The fan shape is modeled with three kinds of shape by varying the radius of the fan blade. By the results of analysis, the flow at Model I is more uniform than Model II or III. And the displacement at Model I is less than Model II or III. As the flow resistance of cooling fan at Model I decreases more than Model II or III, the efficiency becomes better.

• Proceeding of EDISON Challenge
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• 2012.04a
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• pp.109-112
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• 2012

선박의 저항을 추정하는 일은 선박설계에 있어 가장 기본적인 작업이다. 그러나 선박의 크기는 매우 크기 때문에 일반적으로 모형선 실험을 통해 선박의 저항을 추정한다. 이 때, 모형선 실험은 Froude 수를 기준으로 수행하게 되는데 이 때문에 모형선과 실선의 Reynolds 수가 서로 다른 영역에 놓이게 된다. 따라서 모형선 실험에서 얻어진 데이터를 실선에 그대로 적용할 수 없기 때문에 모형선-실선 저항추정법을 사용하게 된다. 본 연구에서는 이러한 모형선-실선 저항추정법에 사용되고 있는 2 차원 외삽법을 살펴보고 이 기법에 사용되고 있는 ITTC 마찰저항곡선을 등가평판 주위의 유동장 해석결과와 비교하였으며 ITTC 마찰저항곡선에 대해 고찰하였다.

• Journal of the Korean Society of Marine Environment & Safety
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• v.20 no.4
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• pp.419-425
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• 2014

The current work investigated the variation of numerical solutions according to the grid number, the distance of the first grid point off the ship surface, turbulence modeling and discretization. The subject vessel is KVLCC. A commercial code, Gridgen V15 and FLUENT were used the generation of the ship hull surface and spatial system and flow computation. The first part of examination, the effect of solutions were accessed depending on the grid number, turbulence modeling and discretization. The second part was focus on the suitable selection of the distance of the first grid point off the ship surface: $Y_P+$. When grid number and discretization were fixed the same value, the friction resistance showed differences within 1 % but the pressure resistance showed big differences 9 % depending on the turbulence modeling. When $Y_P+$ were set 30 and 50 for the same discretization, friction resistance showed almost same results within 1 % according to the turbulence modeling. However, when $Y_P+$ were fixed 100, friction resistance showed more differences of 3 % compared to $Y_P+$ of 30 and 50. Whereas pressure resistance showed big differences of 10 % regardless of turbulence modeling. When turbulence modeling and discretization were set the same value, friction, pressure and total resistance showed almost same result within 0.3 % depending on the grid number. Lastly, When turbulence modeling and discretization were fixed the same value, the friction resistance showed differences within 5~8 % but the pressure resistance showed small differences depending on the $Y_P+$.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.15 no.8
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• pp.4707-4712
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• 2014

Considerable fuel in cars is consumed by air resistance. The flow resistance against the air stream was analyzed by flow analysis near the passenger car body. In this study, the models were used were cars available on the real market. Two velocities entered into inlet plane of flow were 80 km/h and 110 km/h using the flow analysis of CFX. As the study method, the velocity of air flow near the car and the pressure on the rear part of car body were investigated at the driving of car. The shapes of the study models were models 1 and 2, and the flow streams were four cases of 1, 2, 3, and 4. In case 1 among the four cases, the maximum pressure ($1.017{\times}10^5Pa$) on the rear part was highest and the maximum velocity (43.81m/s) of air flow near car body was fastest. The air drag force in the case of high speed (110km/h) driving a passenger car was higher than that of a normal driving speed (80km/h). The drag force at wide section area of the car body becomes higher than the narrow section area. The shape of the car body can be effectively designed to reduce the air resistance using the study results of this analysis.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2006.05a
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• pp.327-330
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• 2006

Numerical simulations were carried out to investigate the base drag characteristics of a base bleed projectile with a central propulsive jet by considering the base homing process. Overall fluid dynamic process is modeled by Wavier-Stokes equations for reacting flows with two-equation $k-\omega$ SST turbulence closure. The combustion process is modeled by finite-rate chemistry with a given partially burned exit condition of the BBU (base-bleed unit). Besides the demonstrating the capability of the present CFD solver for the base drag and the interaction of the base flow with a rocket plume, present study gives an insight into the fluid dynamics and the combustion process of the hybrid-propulsion projectile.