• 유체기계공업학회:학술대회논문집
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• 유체기계공업학회 2004년도 유체기계 연구개발 발표회 논문집
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• pp.140-150
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• 2004

In this study, the effect of relative position of the blade for the fixed vane has been investigated on blade surface heat transfer. The experiments were conducted in a low speed stationary annular cascade, and heat transfer of blade was examined for six positions within a pitch. Turbine test section has one stage composed of sixteen guide vanes and blades. The chord length of the tested blade is 150 mm and the mean tip clearance of the blade having flat tip is about $2.5\%$ of the blade chord. For the detailed mass transfer measurements on the blade surfaces, a naphthalene sublimation technique was used. The inlet flow Reynolds number is fixed to $1.5{\times}10^5$. Complex heat transfer characteristics are observed on the blade surface due to various flow characteristics, such as separation bubble, relaminarization, transition to turbulence and leakage vortices. The distributions of velocity and turbulence intensity change significantly with the relative position due to the blockage effect of the blade. This causes the variation of heat transfer patterns on the blade surface. The results show that the flow near the leading edge get highly disturbed and deflected toward the either side of the blade when the blade leading edge is positioned close to the trailing edge of the vane. Therefore, separation bubble disappears on the pressure side and overall heat transfer on the relaminarization region is increased. But, due to reduced tip gap flow at the upstream region, the effect of leakage flow on the upstream region of the blade surface is weakened. Thus, the heat transfer characteristics significantly change with the blade positions.

• Biotechnology and Bioprocess Engineering:BBE
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• 제11권6호
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• pp.484-488
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• 2006

Alteration of illumination with optimum carbon dioxide fixation-based curve in this research successfully enhanced the $CO_{2}-fixation\;(q_CO_{2}$ capability of Chlorella vulgaris Buitenzorg cultivated in a bubble column photo bioreactor. The level of $CO_{2}$ fixation was up to 1.91 times that observed from cultivation with intensification of illumination on an optimum growth-based curve. During 144 h of cultivation, alteration of light intensity on an optimum $CO_{2}-fixation-based$ curve produced a $q_CO_{2}$ of $12.8\;h^{-1}$. Meanwhile, alteration of light intensity with a growth-based curve only produced a $q_CO_{2}$ of $6.68\;h^{-1}$. Increases in light intensity based on a curve of optimum $CO_{2}-fixation$ produced a final cell concentration of about 5.78 g/L. Both cultivation methods were carried out under ambient pressure at a temperature of $29^{\circ}C$ with a superficial gas velocity of $2.4\;m/h(U_{G}$. Cells were grown on Beneck medium in a 1.0 L Bubble Column Photo bioreactor illuminated by a Phillips Halogen Lamp (20 W/12 V/50 Hz). The inlet gas had a carbon dioxide content of 10%.

• 한국산학기술학회논문지
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• 제10권7호
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• pp.1446-1452
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• 2009

직경 340mm, 높이 195mm의 원심유동층에서 10.5${\mu}m$와 21.5${\mu}m$의 평균직경을 갖는 $Al_2O_3$를 유동물질로 하여 400, 600, 800, 1000rpm으로 기포의 거동을 규명하고자 2중사진 촬영에 의해 유동가시화현상을 실험하였다. 실험결과, 본 실험 범위에서 원심유동층에서 기포의 거동은 회전수에 영향을 받는 것을 알 수 있었으며, 회전수가 증가함에 따라 기포가 발생하기 시작하는 속도는 증가하였으나 기포의 직경은 감소하는 것을 알 수 있었고 기포의 크기는 상대적으로 작게 나타났다.

• 대한기계학회논문집B
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• 제28권8호
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• pp.895-901
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• 2004

Single-phase convection and nucleate boiling heat transfer were locally investigated for confined planar water jets. The detailed distributions of the wall temperature and the convection coefficient as well as the typical boiling curves were discussed. The curve for the single-phase convection indicated the developing laminar boundary layer, accompanied by monotonic increase of the wall temperature in the stream direction. Boiling was initiated from the furthest downstream as heat flux increased. Heat transfer variation according to the streamwise location was reduced as heat flux increased enough to create the vigorous nucleate boiling. Velocity effects were considered for the confined free-surface jet. Higher velocity of the jet caused the boiling incipient to be delayed more. The transition to turbulence precipitated by the bubble-induced disturbance was obvious only for the highest velocity, which enabled the boiling incipient to start in the middle of the heated surface, rather than the furthest downstream as was the case of the moderate and low velocities. The temperature at offset line were somewhat tower than those at the centerline for single-phase convection and partial boiling, and these differences were reduced as the nucleate boiling developed. For the region prior to transition, the convection coefficient distributions were similar in both cases while the temperatures were somewhat lower in the submerged jet. For single-phase convection, transition was initiated at $x/W{\cong}2.5$ and completed soon for the submerged jet, but the onset of transition was retarded to the distance at $x/W{\cong}6$ for the fee-surface jet.

• Korean Chemical Engineering Research
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• 제47권2호
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• pp.195-202
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• 2009

선택적 고체순환이 가능한 2탑 유동층 공정 개발을 위한 기초연구로 금속 망이 장착된 입자크기분리 시스템에 의해 입자크기 차이를 이용하여 고운입자와 굵은입자를 분리할 수 있는 고체분리기를 개발하였으며 고체분리속도에 미치는 유속, 고체분리기의 설치높이 및 분리면적의 영향을 측정 및 고찰하였다. 고체분리기에 의한 고체분리속도는 기체유속, 고체분리기의 설치높이, 분리면적이 증가함에 따라 증가하였다. 기체유속 및 고체분리기 설치높이 증가에 따른 고체분리속도의 변화경향은 기포크기의 변화경향과 유사하였다. 본 연구에서 개발한 고체분리기를 이용하여 굵은입자($212{\sim}300{\mu}m$)와 고운입자($63{\sim}106{\mu}m$)의 분리가 가능하였으며 고체분리속도는 4.4~127 g/min의 범위를 나타내었다. 개발된 고체분리기를 회수증진 수성가스변환 공정에 적용하여 선택적 고체순환이 가능한 2탑 유동층 공정구성을 제안하였다.

• 대한조선학회논문집
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• 제34권4호
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• pp.42-52
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• 1997

수중램제트(underwater ram-jet)는 램흡입부(ram intake), 혼합실(mixing chamber) 및 노즐(nozzle)로 구성되어 있으며, 램흡입부로 유입된 작동유체는 압력이 증가되며 이 증압된 작동유체에 혼합실로부터 고압공기를 분사하여 기 액이상류를 형성하여 노즐을 통과하면서 대기압까지 팽창을 하여 작동유체를 고속으로 가속시켜 노즐출구로부터 추력을 얻는 방식으로 차세대 초고속 선박추진장치이다. 본 연구에서는 80노트를 낼 수 있는 선내관통형(buried type vessel) 램제트의 최적 노즐형상데이터를 이용하여 제반변수(벽마찰계수, 가스속도, 기포반경, 대기온도, 질량유량비, 디퓨저면적비, 작동유체의 속도구배)의 변화가 추진특성에 미치는 영향을 파악하였다.

• 대한기계학회논문집A
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• 제29권1호
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• pp.67-73
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• 2005

The paper presents a single-heater microfluid injector, whose ejected droplet volume is adjusted by digital current path control for a single microheater. The previous droplet volume adjustable methods have used the digital current control for multiple heaters or the analog current control for a single heater, while the present method uses the digital current control for a single microheater. Two different microinjectors, having a rectangular heater and a circular hearter, are designed and fabricated in the chip area of $7.64\;mm{\times}5.26\;mm$. The fabricated microinjectors have been tested and characterized for the number, size, shape and lifetime of the generated bubbles as well as for the volume and velocity of the ejected droplets. The input power for the rectangular heater and the circular heater has been varied in the ranges of $8.7{\sim}24.9{\mu}W\;and\;8.1{\sim}43.8{\mu}W$, respectively. The projected area of the generated bubble has been changed in the ranges of $440{\sim}l,3600{\mu}m^2\;and\;800{\sim}3,300{\mu}m^2$ for the rectangular heater and the circular heater, respectively. The microinjector with the rectangular heater ejects three discrete levels of the droplet in the volume range of $9.4{\sim}20.7pl$ with the velocity range of $0.8{\sim}1.7m/s$, while the microinjector with the circular heater achieves five discrete levels of the droplet in the volume range of $7.4{\sim}27.4pl$ with the velocity range of $0.5{\sim}2.8m/s$.

• 한국산업융합학회 논문집
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• 제25권4_2호
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• pp.637-644
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• 2022

In this study, the flow characteristics according to the shape of the vortex nozzle was studied by numerical analysis and the amount of microbubble generation was measured experimentally. The shape of the vortex nozzle is cylindrical, diffuser, and conical type. The axial fluid velocity in the induced tube gradually increased from the inlet to the outlet. In particular, the fluid velocity in the nozzle part increased rapidly. The velocity distribution of the fluid at the inlet of the induced tube showed that the flow rotates counterclockwise in the outer region and the inner center of the induced tube. At the outlet of the induced tube, the cylindrical and conical type showed rotational flow, and the diffuser type showed irregular turbulent flow. The dimensionless pressure ratio 𝜂 of the inner region of the induced tube was lower than that of the outer region. Also, 𝜂 near the outlet of the induced tube in cylindrical and conical type showed a similar tendency to the inlet area. At the outer region of inlet of induced tube, intense vorticity was observed on the wall and in lower region. At the inner region of inlet of induced tube, intense vorticity was observed on the inner wall of the induced tube and in the central region of the inlet of the induced tube. At the outlet of induced tube, in the case of the cylindrical and conical type, intense vorticity was observed near the inner wall, the diffuser type showed irregular strong vorticity inside the tube. The total number of bubbles measured was the most in the cylindrical type, and the microbubbles less than 50mm occurred the most in the conical type.

• Korean Chemical Engineering Research
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• 제54권5호
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• pp.678-686
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• 2016

본 연구에서는 내경 0.3 m, 높이 2.4 m인 기-고 유동층 반응기 내에서 수직 방향의 내부 구조물과 shroud 노즐 분산판이 기포 흐름에 미치는 영향을 CPFD (Computational Particle-Fluid Dynamics)를 이용하여 모델링을 수행하였다. 층 물질로는 Metal-grade 실리콘 입자(MG-Si)가 사용되었으며 $d_p=149{\mu}m$, ${\rho}_p=2,325kg/m^3$, $U_{mf}=0.02m/s$이다. 전체 층물질의 양은 75 kg이며 정적층(static bed) 높이는 0.8 m이다. 수직 내부 구조물이 기포 상승속도에 미치는 영향을 파악하였다. 내부 구조물이 분산판으로부터 0.45 m 높이에 설치되었을 때 기포의 분쇄가 일어났다. 유동층의 압력강하 및 수직 고체체류량 분포는 내부 구조물의 영향을 크게 받지 않는 것으로 나타났다. 하지만 내부 구조물이 제트에 너무 가까운 경우 기포가 분쇄되지 않고 내부 구조물을 우회하여 상승하였으며 내부 구조물이 없는 경우나 0.45 m 높이에 설치된 경우에 비해 더 빠른 속도로 상승하였다.

• 한국항공우주학회지
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• 제31권7호
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• pp.15-25
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• 2003

진동하는 에어포일의 근접후류 특성을 조사하기 위한 실험적 연구가 수행되었다. NACA 4412에어포일은 1/4 시위 지점을 중심으로 조화적으로 피칭운동을 하고, 순간받음각이 +6$^{\circ}$에서 -6$^{\circ}$까지 진동하도록 하였다. 진동하는 에어포일의 근접후류에서의 평균속도를 측정하기 위하여 열선풍속계를 사용하였다. 본 연구에서 자유류의 속도는 3.4, 12.4, 26.2 m/s이다. 이러한 자유류 속도에 따른 시위 레이놀즈수는 $R_N$=5.3${\times}10^4$, 1.9${\times}10^5$, 4.1${\times}10^5$이고, 무차원 진동수는 K=0.1이다. 레이놀즈수가 진동하는 에어포일의 근접후류에 미치는 영향을 나타내기 위하여 축방향 위상평균 속도분포를 제시하였다. 본 측정에서 모든 경우에 속도결손은 $R_N$=5.3${\times}10^4$인 경우에 아주 크고, $R_N$=1.9${\times}10^5$과 4.1${\times}10^5$인 경우에는 작다는 것을 관찰 할 수 있었다. 이와 같이 위상평균속도의 커다란 차이는 $R_N$=5.3${\times}10^4$과 1.9${\times}10^5$ 사이에 있다는 것을 관찰하였다. 따라서 본 연구는 진동하는 에어포일의 근접후류에서의 레이놀즈수의 임계값이 5.3${\times}10^4$에서 1.9${\times}10^5$ 범위에 존재한다는 것을 보여준다.