• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2000.11a
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• pp.13-13
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• 2000

램제트 엔진에 대한 기초 연구로서 양쪽 대칭의 공기 흡입구를 갖는 2차원 형태의 램제트엔진 연소기를 제작하여 그 특성을 분석하였다. 실험은 흡입공기의 연소실내 유입각도와 연소실내의 도움 위치에 따른 연소실 형상을 바꾸어가며 연소기내의 유동특성을 살펴보았다. 이를 위하여 고속 유동장의 2차원 평면 속도 분포를 측정할 수 있는 two color PIV 기법을 개발하였다. 이 기법은 다른 색의 두 레이저빔을 사용하여 방향성의 문제를 해결하며, 이미지의 색 분리에 따른 거의 완벽한 cross-correlation이 가능하며 높은 single-to-noise 비를 얻게 됨으로써 dynamic range의 증가가 가능해지며, 조사 영역 안에 존재해야 하는 입자 쌍의 수가 줄어들게 된다.(중략)

• Transactions of the Korean Society of Mechanical Engineers
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• v.14 no.4
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• pp.927-936
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• 1990

본 연구에서는 정4각 단면덕트의 입구영역에서 층류 정상유동의 유동특성을 이론적 및 실험적인 방법으로 속도파형과 속도분포를 얻어서 유동이 발달되고 있는 유 동특성과 입구길이를 규정하였다. 이론적인 방법으로는 덕트입구영역에서 공기유동 에 대한 운동량방정식을 유도한 후, 운동량방정식 중의 비선형인 대류항을 선형화시켜 서 Laplace변환으로 속도 분포식의 해를 구하였고, 실험적인 방법으로는 시험덕트의 크기가 40*40*4,000nm(가로*세로*높이)인 정 4각단면덕트에 송풍기로 공기를 흡입 하여 정상유동을 얻었고, 열선유속계에 의하여 속도파형과 속도분포 등의 측정한 결과 를 이론식과 비교검토하였다.

• Journal of Energy Engineering
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• v.14 no.4 s.44
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• pp.213-218
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• 2005

In order to understand the heat and mass transfer characteristics of humid airflow in frosting conditions, a flat plate of aluminum with cooling modules located in the central part of the plate was used. A microscope system (resolution of 0.05 mm) was used for the measurement of local thickness of frost at seven points along the plate in the flow direction. For the total mass of frost at each test operation, an electronic balance (resolution of 1 mg) was used. The local frost thickness distributions far various test conditions were presented along with the frost mass data measured at the given operating times. The effect of humidity and velocity of humid air on frosting were analyzed.

• Transactions of the Korean Society of Mechanical Engineers
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• v.15 no.1
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• pp.299-307
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• 1991

A unified correlation of the interfacial friction factor for air-water and steam-water flows in inclined rectangular channels has been developed. The correlation was expressed in the form of a power law of the liquid and the gas Reynolds number, and the liquid-to-gas viscosity ratio. In addition, a relation between the equivalent roughness and the intensity of wave height fluctuation of the interface has been investigated. A new dimensionless intensity of fluctuation including a liquid film Reynolds number is proposed. It has been shown that the dimensionless equivalent roughness, which is calculated from the Nikuradse equation, can be uniquely related to this dimensionless intensity of fluctuation for both air-water and steam-water flows.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.34 no.10
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• pp.61-70
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• 2006

A Supersonic air intake model was designed for the high performance ramjet and dual-mode scramjet engine to operate at Mach 4 flight condition. The air intake was tested in the blowdown-type wind tunnel of Kyushu University to identify the internal flow characteristics corresponding to the flight parameters such as the back pressure, angle of attack and angle of yaw. Flow visualization was achieved by the Schlieren and oil flow visualization techniques. The intake performance was analyzed quantitatively based on the surface pressure and total Pressure measurements. The experimental results were compared with the computational fluid dynamics results. The present study exhibits the fundamental but rarely found experimental results of the high Mach number supersonic air intake.

• Journal of the Korean Society of Propulsion Engineers
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• v.7 no.4
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• pp.39-45
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• 2003

Of the various means for active trajectory correction, a thrust vector control system represents the only principle independent of missile external forces so that this method is operative. The purpose of this study is to analyze the characteristic of jet vane TVC(Thrust vector control) system among mechanical jet deflection. To ensure high performance leading edge shape, aspect ratio and ablated condition is optimized. Supersonic flow system, jet vanes and nozzle with Mach number 2.88 and under expansion ratio 2 were designed to study aerodynamic characteristics of leading edge shape, aspect ratio and ablated conditions.

• Journal of Energy Engineering
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• v.25 no.4
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• pp.152-158
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• 2016

Nitrogen oxide is generated by the chemical reaction of oxygen and nitrogen in higher temperature environment of combustion facilities. The NOx reduction equipment is generally used in the power plant or incineration plant and it causes enormous cost for the construction and maintenance. The flue gas recirculation method is commonly adopted for the reduction of NOx formation in the combustion facilities. In the present study, the computational fluid dynamic analysis was accomplished to elucidated the cold flow characteristics in the flue gas recirculation burner with coanda nozzles in the flue gas recirculation pipe. The inlet and outlet of flue gas recirculation pipes are directed toward the tangential direction of circular burner not toward the center of burner. The swirling flow is formed in the burner and it causes the reverse flow in the burner. The ratio of flue gas recirculation flow rate with the air flow rate was about 2.5 for the case with the coanda nozzle gap, 0.5mm and it was 1.5 for the case with the gap, 1.0mm. With the same coanda nozzle gap, the flue gas recirculation flow rate ratio had a little increase when the air flow rate changes from 1.1 to 2.2 times of ideal air flow rate.

• Proceedings of the Korea Air Pollution Research Association Conference
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• 2001.11a
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• pp.97-98
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• 2001

폐기물 소각로는 주입 폐기물의 성상이 균일하지 못하므로 폐기물의 불완전 연소에 의한 유해중간 생성물들이 생성되므로 논란이 되어왔다. 이를 제어하기 위해서는 공기량, 공기 주입방법, 공기 예열온도등에 운전조건들의 선정이 매우 중요하다. 이를 위해 진행되어온 연구는 크게 실험적 방법과 수치 해석적 방법의 두 범주로 나뉘어진다. 이에 본 연구에서는 수치해석적 방법으로 광주 상무신도심에 설치 가동중인 200톤/일 용량의 소각로내의 열유동 현상을 해석하기 위하여 고체 폐기물이 매우 빠르게 탈휘(devolatilization)되는 것으로 가정, 메탄가스로 단순화(Chen et al, 1999)하였다. (중략)

• Journal of Advanced Marine Engineering and Technology
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• v.40 no.4
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• pp.330-335
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• 2016

In this study, aerodynamic characteristics of the blades of a helical-type vertical axis wind turbine(VAWT) have been investigated. For this purpose, a 100-W helical-type vertical axis wind turbine was designed using a design formulae, and a 3D computational fluid dynamics analysis was performed considering wind tunnel test conditions. Through the results of the analysis, the aerodynamic power output and flow characteristics of a helical blade were confirmed. In order to validate the aerodynamic power output obtained through the analysis, a wind tunnel test was performed by using a full-scale helical-type vertical axis wind turbine. The 3D analysis technique was validated by comparing its results with those obtained from the wind tunnel test.

• Journal of the Korean Association of Geographic Information Studies
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• v.23 no.3
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• pp.220-235
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• 2020

Heat wave generation in cities is basically affected by global warming, but it is further exacerbated by the impact of artificial heat emission and heat accumulation in the city. In particular, the effects of urban heat waves directly affect the occurrence of tropical nights. Basically, however, the choice of countermeasures against tropical nights is very limited compared to the daytime heat wave response. The purpose of this study was to analyze the characteristics of cold air flow at night as a countermeasure against tropical nights in Daegu Metropolitan City and to suggest its spatial applicability. As a research method, the spatial characteristics (flow velocity, flow rate, flow direction and range) of cold air flow in Daegu were quantitatively analyzed using KLAM_21, a cold air flow analysis program. As a result of the analysis, it was found that cold air generation and flow in the surrounding mountains of Daegu Metropolitan City was very active, but the inflow was limited to the urban area, which has tropical nights. However, it has been shown that the flow of cold air flowing from the surrounding mountains is very active in some urban areas, so it has spatial conditions that are very effective in countering tropical nights. If these spatial conditions are used for the urban planning, it will be very useful to develop countermeasures for tropical nights.