• 한국지반공학회:학술대회논문집
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• 한국지반공학회 2008년도 춘계 학술발표회 초청강연 및 논문집
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• pp.778-783
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• 2008

In this paper, numerical method was calculated on evaluation of underground ventilation system to keep servicing a fresh air. The tunnel length for simulation is 18.2 km with various located seven ventilation shaft. Generally, owing to thermal generation in cable tunnel under about 50 m depths, cable tunnel ventilation system is more important than that of other tunnels. So, we conducted that the effects of ventilation systems was simulated depending on the difference of electrical power tunnel length, the number of shaft tunnel, forced ventilation and duct was or not. Test results show that the main conditions in order to enhance the underground cable tunnel are that ventilation systems have to be designed with forced ventilation and with duct.

• 한국안전학회지
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• 제16권4호
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• pp.1-6
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• 2001

An experimental study was carried out to investigate the emission characteristics of LP gas burner for the Practical combustion conditions including fm voltage, inlet area, gas Pressure, emission resistance, duct length and height. The result shows that CO is almost remains constant for the emission fan voltage, but significantly increases with the reduction rate of air inlet, up to 3000ppm at 50% of reduction rate. Also, the variation of gas pressure has no effect to CO of gas boiler due to its governor which controls gas pressure secondly, but it gives an rapid increase of CO for the gas range. The emission resistance test shows that CO is suddenly increased with the reduction rate of emission duct above 70% and main burner is stopped at 90%. The reverse wind test shows that CO is suddenly increased with the air velocity above 7m/s and main burner is stopped at 9m/s. The more horizontal length of emission duct is long and the vertical height is low, CO is infinitesimally increased.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2000년도 추계학술대회논문집B
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• pp.397-403
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• 2000

In the present study, flow characteristics of turbulent pulsating flow in a square-sectional $180^{\circ}$ curved duct were experimentally investigated. Experimental studies for air flows were conducted to measure axial velocity and wall shear stress distributions and entrance length in a square-sectional $180^{\circ}$ curved duct by using the LDV with the data acquisition and the processing system. The experiment was conducted in seven sections from the inlet (${\phi}=0^{\circ}$) to the outlet (${\phi}=180^{\circ}$) at $30^{\circ}$ intervals of the duct. The results obtained from the experimentation were summarized as follows ; (1) When the ratio of velocity amplitude ($A_1$) was less than one, there was hardly any velocity change in the section except near the wall and any change in axial velocity distributions along the phase. When the ratio of velocity amplitude ($A_1$) was 0.6, the change rate of velocity was slow. (2) Wall shear stress distributions of turbulent pulsating flow were similar to those of turbulent steady flow. The value of the wall shear stress became minimum in the inner wall aid gradually increased toward the outer wall where it became maximum. (3) The entrance length of turbulent pulsating flow reached near the region of bend angle of $90^{\circ}$, like that of turbulent steady flow. The entrance length was changed by the dimensionless angular frequency (${\omega}^+$).

• 산업기술연구
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• 제19권
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• pp.59-65
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• 1999

This study is to analyze turbulent flow over a backward-facing step in a rectangular duct. The side wall effects on the internal flow were determined by varying the aspect ratio(defined as the step span-to-height ratio) from 1 to 20. In the flow behind a backward-facing step, separation, recirculation and redeveloping is occurred frequently. These phenomena appear in a particular variation by varying the aspect ratio. The results show that the aspect ratio has an influence on the velocity and reattachment length. When the AR is increased, the reattachment length is increased. For 6 over aspect ration, the rate of increase is decreased. The length of recirculation in the upper corner is increased, as the increase of aspect ration. It's width is not changed in the variation of aspect ration. The transverse, streamwise and spanwise velocities were decreased along the flow down stream of the step.

• 한국산학기술학회논문지
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• 제17권10호
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• pp.618-627
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• 2016

본 연구는 정사각형 단면 $180^{\circ}$ 곡관 내의 유동특성을 파악하기 위해 RSM 난류모델을 이용하여 작동유체, 입구의 공기속도, 관내의 표면조도, 곡률반경 및 수력직경 등의 다양한 유동인자를 변경하여 각도 위치별 속도분포특성을 수치해석을 통하여 고찰하였다. CFD 해석시 경계조건은 공기와 물의 입구온도를 288 K, 293 K로 설정하였고, 입구의 공기속도, 관내의 표면조도, 곡률반경 및 수력직경은 각각 3~15 m/s, 0~0.001 mm, 2.5~4.5D, 70~100 mm로 적용하여 해석을 수행하였다. 그 결과를 정리하면, 작동유체의 유동특성은 유체의 점성력 차이로 속도분포가 크게 달라짐을 알 수 있었고, 곡관부 내에서의 최대 속도프로파일은 $90^{\circ}$ 단면위치에서 X/D=0.8 영역으로 나타났으며, $180^{\circ}$ 단면위치에서는 Y/D=0.8 영역으로 나타났다. 그리고 관내의 표면조도가 낮고, 곡률반경이 클수록 속도변화율은 크게 변하여 나타냈다. 또한 곡관후류의 직관부에서 유동편차가 안정화되는 직관거리는 L/D=30 영역에서 나타내어 유량 계측시 유효한 측정위치로 잘 제시할 수 있었으며, 수력직경에 따라 곡관후류 직관부의 표준편차특성은 동일한 유속일 때 최소의 편차영역은 대체로 직관거리 L/D=15~30 범위로 나타났다.

• 한국수소및신에너지학회논문집
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• 제24권4호
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• pp.326-333
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• 2013

This paper presents the performance enhancement of a double-inlet centrifugal blower by the shape optimization of an inlet duct. Two design variables, a length of anti circulation vane and an angles of inlet guide, are introduced to improve the inlet flow uniformity leading to the blower performance. Three-dimensional Navier-Stokes equations are used to analyze the blower performance and the internal flow of the blower. From the shape optimization of the inlet duct of the double-inlet centrifugal blower, the optimal positions of each design variable are determined. Throughout the analysis of sensitivity, it is found that the angle of the inlet guide is more effective than the length of the anti-circulation vane to increase flow uniformity at the outlet of the duct. Efficiency and pressure for the optimal inlet duct shape are successfully increased up to 3.55% and 3.2% compared to those of reference blower at the design flow condition, respectively. Detailed flow field inside the blower is also analyzed and compared.

• 대한기계학회논문집
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• 제19권5호
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• pp.1269-1279
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• 1995

An experimental study is carried out on turbulent diffusion flames stabilized by a circular cylinder in a divergent duct flow. A commercial grade gaseous propane is injected from two slits on the rod as fuel. Flame stability limits, as well as size and temperrature of recirculation zone, are measured by direct and schlieren photographs to clarify the characteristics and structure of diffusion flames and to assess the effect of various divergent angle of duct. The results of the present study are as follows. Temperature in the recirculation zone decreases with increasing divergent angle. The blow-off velocity in parallel duct is higher than that in divergent duct. Critical blow-off velocity is expected to be about 8-12 degree through blow-off velocity pattern. Regardless of divergent angles, the length of recirculation zone is nearly constant, and this length becomes longer with rod diameter. Pressure gradient has an effect on the eddy structure in shear layer behind the rod. With the increase of divergent angle, large scale eddies by dissipated energy in shear layer are split into small scale eddies, and the flame becomes a typical distributedreacting flame.

• 대한기계학회논문집B
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• 제29권5호
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• pp.545-553
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• 2005

In the present study, The characteristics of developing steady laminar flows of a straight duct connected to a $180^{\circ}$ curved duct were examined In the entrance region through experimental measurement. Flow characteristics such as shear stress distributions, pressure distributions and friction coefficient experimentally in a square cross-sectional straight duct by using the PIV system. For the PIV measurement by particles produced from mosquito coils particles. The experimental data were obtained at 9 points dividing the test sections by 400mm. Experimental results can be summarized as follows. Critical Reynolds number, $Re_{cr}$ which indicates transition from laminar steady flow to transition steady flow was 2,150. Shear stress per unit length on the wall was stronger than that in the fully developed flow region. This was attributed to the fact that shear stress and pressure loss in the curvature of a duct were increased. Pressure distributions were gradually decreased irrespective of Reynolds number In the whole test section. This trends were in a good agreement with the reference results. Pipe friction coefficient in the steady state flow region was calculate from method of least squares. The co-relationship between fiction coefficient and Reynolds number was established as follow; ${\lambda}=56/Re$.

• 플랜트 저널
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• 제6권2호
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• pp.62-69
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• 2010

The stability of coal pulverizer in the 800 MW coal-fired plants is vital to maintain their performance. Thus, this study analyzed the uneven abrasion of the deflector and coal spillage due to the air velocity maldistribution in the vane wheel of a bowl-type pulverizer as it is a possible cause for problems of facility using pulverized coal. In addition, air flow in the underbowl of a bowl-type pulverizer was studied to check air velocity maldistribution in the vane wheel using numerical method. In an attempt to correct the maldistribution of air velocity, air flow of the modified duct vane was studied as enlarging the length of the duct vanes installed at the air inlet duct of the pulverizer and increasing the angle of inclination. It was found that modified duct vane make the velocity distribution at the vane wheel uniform. formed by the duct vanes installed at the air inlet duct of the pulverizer and swirling flow is the major factor in making the velocity distribution of vane wheel exit uniform. This can prevent the uneven abrasion of the deflector, which is one of the components inside the pulverizer and coal spillage.

• 대한수의학회지
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• 제34권1호
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• pp.1-7
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• 1994

The distribution of the bile and hepatic ducts within the liver of 24 Korean native cattle were observed. Vinylite solution was injected into common bile ducts on 13 cases for cast preparation. The angiography was prepared in 11 cases which were injected 30% barium sulfate solution into the common bile ducts and then radiographed on X-ray apparatus. The results were summarized as follows; 1. The dorsal, intermediate and ventral ducts of left hepatic lobes, ducts of quadrate lobes, and ducts of papillary process were collected into left hepatic ducts. The dorsal and ventral ducts of right hepatic lobe, ducts of caudate process and papillary process were collected into right hepatic ducts. 2. The bile ducts in the left hepatic lobes were collected into dorsal, ventral and intermediate ducts of left hepatic lobes. The intermediate ducts of left hepatic lobes was absent in some cases(5 cases, 20.83%). 3. In some cases, the ventral ducts of right hepatic lobes were collected into right hepatic ducts directly. 4. The ducts of quadate lobes were collected into left hepatic ducts(8 cases, 33.33%), ventral ducts of left hepatic lobes(13 cases, 54.17%), and dorsal duct of left hepatic lobes, intermediate and ventral ducts of left hepatic lobe, common trunk collected into intermediate and ventral duct of left hepatic lobe and left hepatic duct(1 cases, 4.17%) respectively. 5. The ducts of papillary process were collected into left and right hepatic ducts(12 cases, 50%), left hepatic ducts only(11 cases, 45.83%) or right hepatic duct only(1 cases, 4.17%). 6. The average length of right hepatic ducts was 26.87(6-45.8)mm. The average length of left hepatic ducts was 56.68(6-127)mm. The length of gallbladder was 128.60(104-160)mm on the average. The breadth of gallbladder was 67.16(38.4-153.4)mm on the average. But there was a difference in the length and the breadth according to the quantity of bile. 7. The ramified angles of dorsal, intermediate and ventral ducts of left hepatic lobes, ducts of quadrate lobes, ducts of papillary processes and caudate processes, dorsal and ventral ducts of right hepatic lobes and cystic ducts were 130-170, 160-200, 190-250, 240-300, 90-140, 320-350, 30-100, 270-330 and 240-300 degrees respectively.