• Korean Chemical Engineering Research
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• 제43권4호
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• pp.525-530
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• 2005

상용 순환 유동층 연소로(200 ton steam/hr, $4.97{\times}9.90{\times}28.98m$)의 수관벽에서 전열관의 마모속도를 측정 및 고찰하였다. 전열관의 두께는 초음파 측정방법을 이용하여 측정되었다. Splash 영역에서 윙월을 포함한 모든 수관벽 전열관의 마모속도가 두드러졌다. 전열관의 마모속도는 분배기로부터 높이가 증가함에 따라서 감소한 후 다시 증가하였다. 프리보드 기체출구 부근의 윙월에서는 기체 및 고체흐름의 편향성으로 인한 마모속도의 차이도 나타났다. 윙월의 마모속도는 연소로 단면의 중앙에 위치할수록 크게 나타났다.

• 한국안전학회지
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• 제24권4호
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• pp.74-81
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• 2009

In this study, the seismic performance of RC school buildings which were not designed according to earthquake-resistance design code were evaluated by using response spectrum and push-over analyses. The torsional amplification effect due to plan irregularity is considered and then the efficiency of seismic retrofitting methods such as RC shear wall, steel frame, RC frame and PC wing wall was investigated. The analysis result indicate that the inter-story drift concentrated in the first floor and most plastic hinge forms at the column of the first story. Among the retrofitting methods, the PC wing wall has the highest seismic performance in strength and story drift aspect. Especially, it can make building ductile behavior due to the concentrated inter-story drift at the first column hinge is distributed overall stories. The axial force, shear force and moment magnitude of existing elements significantly decreased after retrofitting. However, the axial and shear force of the elements connected to the additional retrofitting elements increased, and especially the boundary columns at the end of the retrofitting shear wall should be reinforced for assuring the enhancement of seismic performance.

• International Journal of Aeronautical and Space Sciences
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• 제1권1호
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• pp.13-20
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• 2000

The applications of CFD in the design process of a transonic civil transport at Korea Aerospace Research Institute (KARI) are outlined. Three Navier-Stokes solvers, developed at KARI with different grid approaches, are used to predict the aerodynamic coefficients and solve the flowfield of various configurations. Multi-block, Chimera, and unstructured grids are the approaches implemented. The accuracy of the codes is verified for the transonic flow about RAE wing/fuselage configuration. The multi-block code is used to provide the detailed data on the flowfield around a wall interference model with different test section sizes which will be used in establishing the wall interference correction method. The subsonic and transonic flowfields about K100-04A, one of the configurations of a 100-seater transport developed by KARI and Korea Commercial Aircraft Development Consortium (KCDC), are computed to predict the aerodynamic coefficients. The results for the subsonic flow are compared with those of wind tunnel test, and the agreement is found to be excellent. The interference effect of nacelle installation on the wing of K100-04A is also investigated using the unstructured grid method, and about 10% reduction in wing lift is observed. The accuracy of the three developed codes is verified, and they are used as an efficient tool in the design process of a transonic transport.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2008년도 춘계학술대회논문집
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• pp.483-486
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• 2008

Numerical Simulation was performed to investigate the role of vortex generator. Vortex generator installed on the upper surface of the wing, generates vortex flow, mimic the external flow with boundary layer flow and transfer energy from outside to wall boundary. Vortex generator, thus, retards the flow separation and increases the lift and drag of the wing.

• 한국수자원학회:학술대회논문집
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• 한국수자원학회 2008년도 학술발표회 논문집
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• pp.2141-2145
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• 2008

저면에 힌지로 연결된 3종류의 부유 플랩 시스템을 대상으로 수리모형실험을 실시하였다. 이 시스템은 입사파를 반사시키고, 구조적 감쇄 및 점성 감쇄를 이용하여 파랑에너지를 감소시켜 차폐 해역을 제공한다. 다양한 파랑조건에 대하여 파랑의 반사, 전달, 플랩의 회전각 등을 분석하였다. 외해 날개벽을 부착한 형태가 파랑의 전달을 최소화시킬 수 있다.

• 콘크리트학회지
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• 제17권5호
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• pp.51-57
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• 2005

• 한국항공우주학회지
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• 제36권7호
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• pp.621-627
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• 2008

풍동에서 측정된 공력자료에는 풍동벽면의 영향으로 인하여 불가항력적인 오차가 포함되어 있다. 벽면영향이 없는 공력자료를 얻기 위해서는 이러한 원하지 않는 벽면효과를 제거 하여야 한다. 유선곡률 효과는 풍동벽면의 영향으로 유선의 곡률이 자유 흐름의 것과 다르기 때문에 발생한다. 고정익 항공기에 사용되고 있는 전통적인 유선곡률 효과를 보정방법인 Glauert의 보정방법은 회전익 항공기에 적용이 적절하지 않다. 본 논문에서는 로터에 적절한 후류모델을 사용하는 Heyson의 보정방법을 사용하여 로터축 기울어짐 각과 동압을 보정하였다. Heyson 보정방법의 결과를 Glauert 보정방법의 결과와 비교하였다.

• Journal of Ship and Ocean Technology
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• 제11권3호
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• pp.39-50
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• 2007

This study aims the observation of wing-in-ground effect near free surface. Numerical computations are carried out to observe the deformation of free surface and the effects on lift and drag. The detailed flow fields around two- and three-dimensional wings with NACA 0012 section are observed from the results of a commercial CFD program, FLUENT, and the local deformations of free surface are obtained by applying a Rankine panel method. In the present cases, the small deformation of free surface under the wings is observed, but different forces are found between solid wall and free surface when the speed of wings becomes large.

• 대한기계학회논문집B
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• 제33권10호
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• pp.757-766
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• 2009

In the present study, the effect of delta-wing vortex generators(DWVG) on the local heat transfer of the plate fin-oval tube was experimentally analyzed for Reynolds numbers for 2000, 2500 and 3200. The local heat transfer coefficient of the fin surface for four type DWVGs was measured by the naphthalene sublimation technique. As the results, the distribution of the heat transfer coefficient at rear of DWVGs showed longitudinal contours for common flow down DWVGs and wavy contours for common flow up DWVGs. The distribution showed many cell type contours at near wall and downstream for all DWVGs. Compared to case without DWVGs in present experimental tests, all DWVGs showed the best enhancement of heat transfer at Re=2000. Of 4 cases of DWVGs, D type showed the best enhancement of heat transfer.

• 한국지반공학회:학술대회논문집
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• 한국지반공학회 2009년도 세계 도시지반공학 심포지엄
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• pp.809-814
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• 2009

Deep mixing method has been used for ground improvement and foundation system for embankment, port and harbor foundations, retaining wall, and liquefaction mitigations. It has attractive benefits because it is not only improved strength of soft ground but superior for prevention of settlement. However, the quality controls of improved mass affect to the efficiency of the deep mixing method is not properly established. These effects vary depending upon the construction environments and conditions of agitation in consideration of an agitator. The strength and shape of the improved column are not unique and these are affected by mechanical properties of agitators. In this study, in order to investigate the efficiency of deep mixing method for ground improvement on a soft clay ground, experimental studies are performed considering mechanical properties of agitator; the location of exit-hole of admixtures, an angle of mixing wing and a speed of revolution. The experiments are conducted with the simulated apparatus for deep mixing plant that reduced the scale in 1:8 of the real plant. According to the results, the diameter and shape of improved column mass vary depending on the mechanical properties and operating conditions of agitator. Its quality is better when the exit-hole of admixtures is located in the mixing wing, when an angle of mixing wing is large, and when the speed of revolution is rapid.