• 한국산학기술학회논문지
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• 제14권1호
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• pp.485-492
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• 2013

일반과 변형구조의 싸이클론에서 입자흐름의 체류시간분포 특성을 통해 선회강도, 난류성 에디, 벽면 바운싱에 의한 고체흐름의 역혼합과 2단 선회류 약화기의 직경이 집진효율에 미치는 영향을 고찰하였다. 변형구조 싸이클론(S = 13, 15cm)에서 플라이애쉬의 집진효율이 일반 싸이클론보다 높게 나타났다. 변형구조의 싸이클론에서 집진효율은 2단 선회류 약화기의 직경(S)이 13cm에서 가장 높게 나타내었다. 글라스비드의 체류시간분포에 대한 분산과 평균 체류시간은 선회강도와 난류성 에디로 인해서 2단 선회류 약화기의 직경이 증가할수록 증가하였다. 변형구조의 싸이클론에서 고체 흐름의 역혼합은 기체 유입속도가 증가할수록 증가하였고 일반 싸이클론보다 높게 나타났다.

• 상하수도학회지
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• 제26권3호
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• pp.463-469
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• 2012

The efficiency of the flow mixed pump installed within the bell-mouth in the sump is reduced by the flow characteristics of around intakes. Strong submerged vorticies can be successfully suppressed by installing an AVD(anti-submerged vortex device) on the bottom of pump intake channel just below the bell-mouth. Sump model with AVD device basin is designed and the characteristics of submerged vortex is investigated in the flow field by numerical simulation. In this study, a commercial CFD code is used to predict the efficiency of the pump with the AVD installation in the pump station accurately.

• 한국정밀공학회지
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• 제8권4호
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• pp.95-106
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• 1991

A numerical computation of turbulent wirling flow in a stationary pipe is presented in this work. Major concerns of this study are: 1) To approve similarity laws which were verified experimentally. 2) To investigate the effects of curvature modification for the K- .epsilon. model. To account for effects of swirl, Rodi's curvature correction and Kim & Chung's are applied. The governing differential equations for eliptic flow are discretized by control volume formulation method, and the discretized equations are calculated ay line by line TDMA and SIMPLE algorithm. The computational results also satisfy similarity laws which are based on swirl angle as in experiments. And the curvature modification of Rodi improves compuational accuacy than the standard K- .epsilon. model. But such lower order closure models are not adequate for the prediction of this complex flow.

• 산업기술연구
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• 제19권
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• pp.51-57
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• 1999

This research has an object to find out how the position of inlet valve influence swirling and tumbling of turbulence inside the combustion chamber of 4 valve engine. The computational analysis of three dimensional complicated turbulence flow in the cylinder is done by the KIVA-3V program to carry out this object. One use 6 valve positions with the bowl type of piston cavity. The swirl ration and the tumbling ratio of flow filed are evaluated quantitatively to find out how each valve position influence flow phenomena in the combustion chamber during the intake and compression processes.

• 대한기계학회논문집
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• 제18권2호
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• pp.492-501
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• 1994

This study is an analysis of the turbulent diffusion flame with swirl flow and the calculated results are compared with experimental data in case of various swirl numbers and air-fuel rations. The mathematical model is restricted to single-phase, diffusion controlled combustion with swirl flow. Values of local flow properties were obtained by solving appropriate differential equation for continuity, momentum, stagnation enthalpy, concentration, turbulence energy, dissipation rate of turbulence energy, and the mean square of concentration fluctuation. The method is proposed for calculating the local probability of chemical reaction based on the use of the probability density function for the mixture fraction.

• Korean Chemical Engineering Research
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• 제44권5호
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• pp.505-512
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• 2006

직경이 0.102 m이고 높이가 2.5 m인 액체-입자 swirling(나선)흐름 유동층에서 유동 입자의 흐름 및 열전달 특성을 고찰하였다. 액체유속($U_L$), 유동 입자의 크기($d_p$) 그리고 연속상인 액체의 나선 유도흐름 액체량의 비($R_s$)가 유동층 내 유동입자의 체류량 유동층 내부 열원과 유동층간의 총괄 열전달 계수에 미치는 영향을 검토하였다. 액체-입자 나선흐름 유동층에서 입자 체류량은 입자의 크기와 나선유도흐름 액체량의 비가 증가함에 따라서 증가하였으나, 액체유속의 증가에 따라서는 감소하였다. 유동층 내부에서 나선 유도 흐름 액체량의 비가 0.1~0.3인 경우에 유동 입자의 국부체류량은 유동층 중심부에서 큰 값을 나타내었으나, $R_s$의 값이 0.5일 때는 반경 방향 입자 체류량은 거의 균일한 분포를 보이며, $R_s$의 값이 0.7일 때는 유동층 중심부의 입자 체류량이 상대적으로 감소하는 경향을 나타내었다. 유동층 내부열원과 유동층간의 열전달 특성은 열원 표면과 유동층간의 온도차 요동 자료의 위상공간 투영과 kolmogorov 엔트로피 해석으로 고찰할 수 있었으며, 나선 유도 흐름 액체량의 비($R_s$)가 0.1에서 0.5까지 증가할수록 온도차 요동 자료의 위상공간 투영은 점점 안정되고 규칙성이 증대되는 상태를 나타내고, kolmogorov 엔트로피 값은 감소하는 경향을 나타내었다. 열원 표면과 유동층간의 온도차 요동 자료의 kolmogorov 엔트로피 값은 액체의 유속이 증가함에 따라 최대값을 나타내었다. 열원과 유동층간의 총괄 열전달 계수는 액체유속, 층공극률, 나선 유도 흐름 액체량의 비가 증가함에 따라서 최대값을 나타내었으며, 유동 입자의 크기가 증가함에 따라 증가하였다. 내부 열원과 유동층간의 총괄 열전달 계수가 최대값을 나타낼 때의 액체의 유속 조건에서 온도차 요동자료의 kolmogorov 엔트로피의 값도 최대값을 나타내었다. 액체-입자 나선흐름 유동층에서 입자 체류량과 열전달 계수를 무차원군의 상관식으로 나타낼 수 있었다.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2001년도 춘계학술대회논문집E
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• pp.125-130
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• 2001

Experimental and analytical researches have been conducted on the twin-fluid atomizers for better droplet breakup during the past decades. But, the studies on the disintegration mechanism still present a great challenge to understand the drop behavior and breakup structure. In an effort to describe the aerodynamic behavior of the sprays issuing from the internal mixing counter-swirling nozzle, the spatial distribution of axial (U) radial (V) and tangential (W) components of droplet velocities are investigated across the radial distance at several axial locations of Z=30, 50, 80, 120 and 170mm, respectively. Experiments were conducted for the liquid flow rates which was kept constant at 7.95 g/s and the air injection pressures were varied from 20 kPa to 140 kPa. Counter-swirling internal mixing nozzles manufactured at angles of $15^{\circ},\;30^{\circ},\;45^{\circ}$ and $60^{\circ}$ the central axis with axi-symmetric tangential-drilled holes was considered. The distributions of velocities and turbulence intensities are comparatively analyzed. PDPA is installed to specify spray flows, which have been conducted along the axial downstream distance from the nozzle exit. Ten thousand of sampling data was collected at each point with time limits of 30 second. 3-D automatic traversing system is used to control the exact measurement. It is observed that the sprays with all swirl angle have the maximum SMD for on air injection pressure of 20 kPa and 140 kPa with centerline, respectively. The nozzle with swirl angle of $60^{\circ}$ has vest performance.

• 열처리공학회지
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• 제35권1호
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• pp.27-32
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• 2022

Microbubble technology has been widely applied in various industrial fields. Recently, research on many types of microbubble application technology has been conducted experimentally, but there is a limit in deriving the optimal design and operating conditions. Therefore, if the computational fluid dynamics (CFD) analysis of multiphase flow is used to supplement these experimental studies, it is expected that the time and cost required for prototype production and evaluation tests will be minimized and optimal results will be derived. However, few studies have been conducted on multiphase flow CFD analysis to interpret fluid flow in microbubble generators using swirl flow. In this study, CFD simulation of multiphase flow was performed to analyze the air-water mixing process and fluid flow characteristics in a microbubble generator with a dual-chamber structure. Based on the simulation results, it was confirmed that a negative pressure was formed on the central axis of rotation due to the strong swirling flow. And it could be seen that the air inside the suction tube was introduced into the inner chamber of the microbubble generator. In addition, as the high-speed mixed fluid collided with external water sucked by the negative pressure near the outlet, a large amount of microbubbles was ejected due to the shear force between the two flows flowing in opposite directions.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2004년도 제22회 춘계학술대회논문집
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• pp.544-549
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• 2004

하이브리드 로켓 엔진은 일반적으로 저비용ㆍ저공해ㆍ고안전성 등의 이점이 있지만 연료 후퇴 속도가 느려 연비를 제어할 수 없는 문제점이 일어 아직 실용화되지 않고 있다.(중략)

• International Journal of Fluid Machinery and Systems
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• 제4권1호
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• pp.57-66
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• 2011

Radial-vaned air separators show a strong stall suppression effect in an axial flow fans. From a survey of existing literature on the effects and the author's data, a possible mechanism for the significant effects has been proposed here. The stall suppression is suggested to have been achieved by a combination of the following several effects; (1) suction of blade and casing boundary layers and elimination of embryos of stall, (2) separation and straightening of reversed swirling flow from the main flow, (3) induction of the fan main flow toward the casing wall and enhancement of the outward inclination of meridional streamlines across the rotor blade row, thus keeping the Euler head increase in the decrease in fan flow rate, and (4) reinforcement of axi-symmetric structure of the main flow. These phenomena have been induced and enhanced by a stable vortex-ring encasing the blade tips and the air separator. These integrated effects appear to have caused the great stall suppression effect that would have been impossible by other types of stall prevention devices. Thus the author would like to name the device "tip-vortex-ring assisted stall suppression device".