• 한국항공우주학회지
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• 제40권5호
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• pp.385-394
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• 2012

아음속-초음속 패널법(panel method)을 이용하여 항공기의 정적 안정성 미계수와 동적 안정성 미계수 및 조종미계수를 예측할 수 있는 프로그램을 개발하였다. 사용된 코드는 아음속-초음속 소스(source)와 말굽 와류(elementary horse shoe vortex)의 분포를 사용하고, 그 분포의 크기는 얇은 물체 근사(thin body approximation)을 적용하여 간략히 한 경계 조건을 이용하여 계산하였다. 항공기에 부착된 물체 좌표계에서 준정상(quasi-steady) 해석을 통해서 항공기 3축의 댐핑 계수를 예측하였다. 개발된 코드는 삼각날개(delta-wing)의 중립점(neutral point), 롤, 피치 댐핑 계수의 이론치와 비교하여 검증하였다. 마지막으로 F-18의 정적, 동적 안정성 미계수와 조종 미계수를 풍동 시험치와 계산치에 비교하여 개발한 코드의 정확성과 유용성을 확인하였다.

• 대한기계학회논문집
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• 제14권5호
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• pp.1264-1271
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• 1990

본 연구에서는 회전 깃(rotor blade)을 폭 방향과 시위방향으로 많은 평면 페 널(panel)들로 나누어 이에 말굽쇠 형 화류(horseshoe vortex)를 분포시키는 양력면 (lifting surface)으로 대치하고 후류는 깃상의 순환(circulation)분포에 의해 그 크 기가 결정되는 와도(vorticity)를 와류격자로 대치하는 와류격자법(Vortex Lattice Method`VLM)을 사용하여 HAWT의 공기역학적 성능 예측을 시도하였다. 그리고 후류의 형상은 근 후류(near wake)와 원후류(far wake)로 나누어 근 후류는 깃의 후연(trail- ing edge)에서의 속도를 갖고 와선(vortex line)이 움직이게 하여 결정하였고 원 후류 는 반무한대 원형화류 실린더(semi-infinite circular vortex cylinder)로 취급하여 결정하였다.

• 유체기계공업학회:학술대회논문집
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• 유체기계공업학회 2006년 제4회 한국유체공학학술대회 논문집
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• pp.371-374
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• 2006

The objective of this study is to determine the influence of free-stream turbulent intensity on the three-dimensional turbulent flow in a linear turbine cascade. The range of free-stream turbulence intensity considered is 0.7~10%. This study was performed numerically. The results show that the mass averaged loss coefficient increased according to the increase of free-stream turbulence intensity due to increased value of the mass averaged total pressure loss coefficient which was higher than the decreased value of the mass averaged secondary flow loss coefficient. The loss coefficient distribution was changed suddenly at a free-stream turbulence intensity of 10% while the loss coefficient distribution was rarely changed at a lower free-stream turbulence intensity of 5%.

• 대한원격탐사학회지
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• 제30권6호
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• pp.755-767
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• 2014

본 연구에서는 LARIAC2 GIS 자료와 전산 유체 역학(CFD) 모델을 이용하여 미국 캘리포니아 주 Los Angeles의 두 지역(Wilshire blvd. & Carondelet and Broadway & $7^{th}$ St.)을 대상으로 수치 실험을 수행하였다. 두 지역의 상세 도시 대기 흐름의 특성을 조사하기 위해 건물 자료 구축 알고리즘을 통해 벡터 형식으로 제공되는 LARIAC2 GIS 자료로부터 건물 도메인 자료를 추출하였다. 추출한 자료를 CFD 모델 입력 자료로 사용하여, 각 지역의 오전과 오후의 주 풍향과 풍속에 대해 수치 실험을 수행하였다. 도시 지역 내에서는 건물에 의해 국소적인 2차 흐름이 발생하면서 유입류와 비교하였을 때, 풍향과 풍속의 차이가 두드러졌다. 유입류와 평행한 방향으로 형성된 도시 협곡에서는 채널링 효과가 나타나면서 풍속이 국지적으로 증가하였고, 수직인 방향으로 형성된 도시 협곡에서는 연직 방향으로 잘 발달한 소용돌이가 형성되었다. 도시 협곡을 이루지 않은 건물의 풍상측에서는 말편자 소용돌이가 지면 근처에서 형성되었고, 풍하측에서는 재순환 영역이 형성되었다. 이와 같은 2차 순환(도시 협곡 소용돌이, 말편자 소용돌이, 재순환 영역)이 형성된 구역에서는 지면 근처의 풍속이 크게 증가하였다. 평균 풍속과 풍향 변화율을 조사한 결과, 대체적으로 풍속 증가율이 높은 곳에서 풍향 변화율이 비교적 낮았고 풍속 감소율이 높은 곳에서는 풍향 변화율이 높게 나타났다.

• 대기
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• 제22권1호
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• pp.47-55
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• 2012

The characteristics of flow and pollutant dispersion for fire scenarios in an urban area are numerically investigated. A computational fluid dynamics (CFD) model coupled to a mesoscale weather research and forecasting (WRF) model is used in this study. In order to more accurately represent the effect of topography and buildings, the geographic information system (GIS) data is used as an input data of the CFD model. Considering prevailing wind, firing time, and firing points, four fire scenarios are setup in April 2008 when fire events occurred most frequently in recent five years. It is shown that the building configuration mainly determines wind speed and direction in the urban area. The pollutant dispersion patterns are different for each fire scenario, because of the influence of the detailed flow. The pollutant concentration is high in the horse-shoe vortex and recirculation zones (caused by buildings) close to the fire point. It thus means that the potential damage areas are different for each fire scenario due to the different flow and dispersion patterns. These results suggest that the accurate understanding of the urban flow is important to assess the effect of the pollutant dispersion caused by fire in an urban area. The present study also demonstrates that CFD model can be useful for the assessment of urban environment.

• 대한기계학회논문집B
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• 제26권4호
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• pp.578-586
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• 2002

Flow structures around a rectangular prism have been investigated by using a PIV(Particle Image Velocimetry) technique. A thick turbulent boundary layer was generated by using spires arid roughness elements. The boundary layer thickness, displacement thickness and momentum thickness were 650mm, 117.4mm and 78mm, respectively. The ratio between the model height(40mm) and the boundary layer thickness H/$\delta$, was 0.06. The Reynolds number based on the free stream velocity and the height of the model was 7.9$\times$10$^3$. The PIV measurements were performed at three different wall normal planes. Three recirculation regions at forward facing step, top of the roof and backward facing step are clearly seen and show three dimensional features. Dramatic changes of flow patterns are observed in the wake regions in the different spanwise wall normal planes. Instead of reattachment and recirculation zone, rising streamlines are depicted at the normal planes near the side wall due to the interaction with a rising horse shoe vortex. The peak of turbulent kinetic energy occurs at the separation bubble on top of the roof and the magnitude is 2.5 times higher compared with that of the wake region.

• 한국환경과학회지
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• 제19권11호
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• pp.1423-1436
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• 2010

The effects of meteorological and reclaiming conditions on the reduction of suspended particles are investigated using a computational fluid dynamics (CFD) model with the k-$\varepsilon$ turbulence closure scheme based on the renormalization group (RNG) theory. Twelve numerical experiments with different meteorological and reclaiming conditions are performed. For identifying the meteorological characteristics of the target area and providing the inflow conditions of the CFD model, the observed data from the automatic weather station (AWS) near the target area is analyzed. Complicated flow patterns such as flow distortion, horse-shoe vortex, recirculation zone, and channeling flow appeared due to the topography and buildings in the domain. Specially, the flow characteristics around the reclamation area are affected by the reclaiming height, reclaiming size and windbreak height. Reclaiming height affected the wind speed above the reclaiming area. Windbreak induces more complicated flow patterns around the reclaiming area as well as within the reclaiming area. In front of the windbreak, flow is distorted as it impinges on the windbreak. As a result, upward flow is generated there. Behind the windbreak, a secondary circulation, so called, a recirculation zone is generated and flow is reattached at the end of the recirculation zone (reattachment point). At the lower part of the recirculation zone, there is a reverse flow toward the windbreak. Flow passing to the reattachment point starts to be recovered. Total amounts of suspended particles are calculated using the frictional and threshold frictional velocities, erosion potential function, and the number of surface disturbance. In the case of a 10 m-reclaiming and northerly wind, the amount of suspended particles is largest. In the presence of 5 m windbreak, the friction velocity above the reclaiming area is largely reduced. As a result, the total amount of the suspended particles largely decreases, compared to the case with the same reclaiming and meteorological conditions except for the windbreak The calculated suspended particle amounts are used as the emission rate of the dispersion model simulations and the dispersion characteristics of the suspended particles are analyzed.