• Journal of Advanced Marine Engineering and Technology
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• 제41권4호
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• pp.302-309
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• 2017

격납건물에서 수소폭발이 발생된다면 다중방어벽을 훼손하고 다량의 방사능 물질을 방출시킬 수 있기 때문에 노심용융과 함께 발생되는 수소를 효과적으로 제어하고 제거해야 하지만 사고 원인의 다양성과 수소분포, 거동의 불규칙성 때문에 폭발 저감을 위한 대책마련이 쉽지 않다. 본 논문에서는 가장 넓게 사용되는 수소저감 기술인 피동촉매형수소재결합기(PAR)의 수소저감 효율을 높이기 위해 외부 유동을 고려한 가이드 구조에 관하여 연구하였다. 2단 촉매 PAR 내부형상을 기본으로 하여 PAR 외부에 가이드를 부착하였을 때 유체의 거동과 수소저감효율에 대해서 해석을 수행하였다. 유동이 아래에서 위로 올라가는 경우 가이드 높이 150mm, 촉매와 가이드 직접 부착, 가이드 각도가 $60^{\circ}$인 구조가 최적으로 판단되며 유동이 옆에서 불어오는 경우 촉매와 가이드 거리 100mm인 구조가 최적으로 판단되고, 유동이 위에서 아래로 내려오는 경우 직접부착, 높이 50mm 가이드 구조가 최적으로 판단된다.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2011년도 춘계학술대회 논문집
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• pp.785-786
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• 2011

• 한국유체기계학회 논문집
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• 제15권6호
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• pp.25-30
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• 2012

Renewable energy has been interested because of fluctuation of oil price, depletion of fossil fuel resources and environmental impact. Amongst renewable energy resources, hydropower is most reliable and cost effective way. In this study, to develop a new type of micro hydro turbine which can be operated in the range of very low specific speed, a cross-flow hydro turbine with simple structure is proposed. The turbine is designed to be used at the very low specific speed range of hydropower resources, such as very high-head and considerably small-flow rate water resources. CFD analysis on the performance and internal flow characteristics of the turbine is conducted to obtain a practical data for the new design method of the turbine. Results show that optimized arrangement of guide vane angle and inner guide angle can give contribution to the turbine performance improvement.

• 한국컴퓨터정보학회논문지
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• 제19권2호
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• pp.161-171
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• 2014

본 논문에서는 CFDRC 사의 상용 CFD 소프트웨어인 CFD-ACE+로 전산유체역학 기법을 적용하여 수치 해석을 수행하여 배연탈황 설비에서 Induced Draft Fan(I.D.Fan) 출구부터 Booster Up Fan(B.U.Fan) 입구까지 난류 유동장과 연소 유동 문제를 모사하여 배기가스 계통 설비의 유동 특성을 해석하였다. 배기가스가 I.D.Fan 출구 ~ B.U.Fan 입구 구간을 적정속도로 균일하게 유동하여 B.U.Fan로 균일하게 유입되도록 하며 압력손실이 적게 발생하도록 설계기준 보일러 부하와 최대연속 정격유량의 보일러 부하에서 이 구간의 안내깃을 검토하였다. 검토한 결과에 대해 CFD 해석을 수행하여 I.D.Fan 출구에서 안내깃을 제거하고 B.U.Fan 입구 전에 안내깃을 보강할 수 있도록 설계를 변경하였다. 배기가스 계통에 변경된 설계를 적용하여 수치모사한 결과에서 배연탈황 설비 내부의 배기가스 압력손실이 줄어들고 유속과 유선이 균일하게 유동할 수 있어 배연탈황 시스템의 효율이 향상한 것을 확인하였다.

• 한국수소및신에너지학회논문집
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• 제31권3호
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• pp.314-321
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• 2020

In this work, a preliminary design of an inlet guide vane and runner for developing a 2.5 kW hydraulic turbine was conducted by using computational fluid dynamic analysis. Three-dimensional Reynolds-averaged Navier-Stokes equations with shear stress transport turbulence model were used to analyze the fluid flow in the hydraulic turbine. The hexahedral grid system was used to construct computational domain, and the grid dependency test was performed to obtain the optimal grid system. Velocity triangle diagram considering the flow angles of the inlet guide vane and runner was analyzed to obtain a basic geometry of the inlet guide vane and runner. Through modification of the preliminary design, the hydraulic performances of the turbine have improved under overall drop conditions. Especially, the efficiency and power of the turbine increased by 0.95% and 1.45%, respectively, compared to those of the reference model.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2004년도 춘계학술대회
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• pp.444-449
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• 2004

The design modification of bottom guide structures of the instrumented capsule, which is used for the irradiation test in the HANARO reactor, was required because of the trouble of the bottom guide arm's pin during irradiation. The previous structure with 3-pin arms was changed into the cone shape of one body. The specimens of the bottom end cap ring with three different sizes (${\Phi}68/70/72mm$) were designed and manufactured. The out-pile tests for the capsule with previous and new three bottom guide structures were performed in the one-channel flow test facilities. In order to evaluate the compatibility with HANARO and the structural integrity of the capsule, a loading/unloading, a pressure drop, a thermal performance, a vibration, and an endurance test were conducted. From out-pile test results, the capsule with the cone shape bottom guide structures was found to be more stable than the previous structure and the optimized size of the bottom guide structure selected was 70mm in diameter. It is expected that the new bottom guide structures will be applicable to all material and special capsules which will be designed and manufactured for the irradiation tests in the future.

• 한국마린엔지니어링학회:학술대회논문집
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• 한국마린엔지니어링학회 2006년도 전기학술대회논문집
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• pp.281-282
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• 2006

In wide angle diffuser, the increasement of cross-sectional area so rapidly cause possibly separate from the diffuser wall and forming areas of backflow. The flow characteristics of wide angle diffuser with guide damper was investigated for three kind of inclined angle($\alpha=7_{\circ},\;10.5_{\circ}\;and\;14_{\circ}$)of guide damper. Judging from the results, guide damper can be used as an effective means of improvement for diffuser performance and inclined angle of $\alpha=10.5^{\circ}$ was through to be the best among three cases.

• 한국신재생에너지학회:학술대회논문집
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• 한국신재생에너지학회 2011년도 추계학술대회 초록집
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• pp.34.2-34.2
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• 2011

Wind guide can be installed on the top of buildings to collect wind. In this study, optimum shape of wind guide is developed, and proposed to combinate with the vertical wind turbine. Impact of parameters for wind guide is analyzed with several cases planned by Taguchi test plan. Front angle, rear angle, and roof angle are selected as key variables and changed into four different levels. By the experimental plan, totally, 64 cases are reduced to 16 cases of analysis. With optimum design of wind guide, the installed vertical axis wind turbines can be operated with maximum power output.

• 항공우주시스템공학회지
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• 제14권1호
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• pp.8-15
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• 2020

본 논문은 위성을 발사장까지 안전하게 운반하기 위해, 열이나 외부 온도가 심하게 변화하는 조건에서 위성 컨테이너 내부 온도를 일정하게 유지할 수 있도록 컨테이너 벽면 및 경계층 단열 설계 방법을 제시하고 위성 운반용 컨테이너 외부 환경에 대한 열 유동 해석 및 위성 내부 열 전달 해석을 통해 위성 컨테이너 내부 온도가 일정하게 유지되는지 분석하였다. 컨테이너 내부 유동 해석을 통해 컨테이너 내 위성 주변의 유동이 원활 한지 유동 분포를 확인하였으며, 보조 팬 및 공조시스템과 특별한 그릴 가이드 구조 설계 안을 제시하고자 한다.

• 한국가시화정보학회지
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• 제3권1호
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• pp.58-62
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• 2005

Flow characteristics at secondary recirculation zone in a liquid fuel ramjet combustor were investigated using CFD and Stereoscopic PIV method. The combustors have two rectangular inlets that form 90 degree each other. Three guide vanes were installed in each rectangular inlet to improve the flow stability. The tested angle of the air intakes was 60 degree. The experiments were performed in the water tunnel test with the same Reynolds number in the case of Mach 0.3 at inlet. The computational and experimental results showed that the secondary recirculation flow occurred at the front junction of inlet main stream and combustor chamber. The size of secondary recirculation regions are increased with approaching closer to the center of the combustor. Since the performance of combustor is closely dependent not only on the main recirculation in the dome region but also on the secondary recirculation flow in a junction region, the optimal angle of the air intakes should be considered the recirculation size as frame holder.