• 제목/요약/키워드: Numerical flow visualization

검색결과 274건 처리시간 0.023초

이산와법에 의한 2원주 주위의 유동장 가시화 (Visualization of flowfield around Two Circular Cylinders by a Discrete Vortex Method)

  • 노기덕;이영훈;손영태
    • 한국가시화정보학회:학술대회논문집
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    • 한국가시화정보학회 2002년도 추계학술대회 논문집
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    • pp.63-66
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    • 2002
  • The Flow patterns around two cylinders in various arrangements were studied by a discrete vortex method. The flow for the surface of each cylinder was represented by arranging bound vortices at adequate intervals. The viscous diffusion of fluid was represented by the random walk method. The vortex distributions, streaklines, timelines and velocity vectors around two cylinders were calculated for centre-to-centre pitch rations of P/D=1.5 and 2.5, attack angles of $\alpha=0^{\circ},\;30^{\circ},\;60^{\circ},\;and\;90^{\circ}$, correspond to the photographs by flow visualization and the flow intereference between two cylinders in var ious arrangements was clearly visualized by a numerical simulation.

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유동가시화를 통한 다중 수중익 덕트 내 유속조절에 대한 연구 (Study on Flow Velocity Control of a Multiple Hydrofoil Duct via Flow Visualization Techniques)

  • 김지훈;;원보름;;고진환
    • 한국가시화정보학회지
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    • 제14권2호
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    • pp.12-17
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    • 2016
  • In this work, we investigate the flow velocity controllability of a diffuser-type multiple hydrofoil duct by experimental and numerical flow visualization approaches. The flow velocity controllability is analyzed by changing the angle of the hydrofoil near the outlet, which is the diffuser, while the incoming flow velocity is 0.6 m/s in the experiment. When the diffuser angle is changed from 0 to 7.5 degree, the maximum velocity inside the duct is varied from 1.35 m/s to 1.52 m/s. Also, it is shown from the numerical analysis that the maximum velocity is varied from 1.09 m/s to 1.17 m/s in the same condition. Thus, the aspect of the acceleration in the duct due to the increase of the diffuser angle is similar between the both approaches. Therefore, the multiple hydrofoil duct can be used to control the flow speed inside the duct for continuously extracting power close to a rated capacity.

소결로 배기가스 재순환 시스템 내의 유체유동 특성 연구 (Fluid-flow Characteristics of Flue-gas-recirculation System in Sintering Plant)

  • 문찬희;김현동;김경천
    • 한국가시화정보학회지
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    • 제16권2호
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    • pp.7-15
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    • 2018
  • The fluid-flow characteristics of flue-gas-recirculation (FGR) system can have a significant effect on system efficiency of a sintering plant. The flow characteristics in the system were investigated. A sintering plant with FGR system was modeled. Numerical visualization was performed and flow characteristics were analyzed. Characteristics of the flow distribution of the branch ducts, the inflow of air into the recirculating hood, and the flow in the hood were discussed. Based on the results three suggestions were proposed: (1) distribution of branch duct flowrate upstream, (2) installation of external air ducts in the hood, and (3) installation of baffles at the hood corners. The suggestions were tested numerical and experimental visualization methods. The suggestions were effective and confirmed to be applicable to the actual sinter plant.

개방형 구조의 진동형 히트파이프의 응축부 길이에 따른 추력 및 유동 가시화 (Thrust and Flow Visualization according to Length of Condenser Section of Open Pulsating Heat Pipe)

  • 손민재;최종욱
    • 한국가시화정보학회지
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    • 제21권3호
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    • pp.57-64
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    • 2023
  • An open pulsating heat pipe operates continuously by inflow and outflow fluids through an open-type condenser. The open pulsating heat pipe is a device capable of obtaining the thrust due to the variation of internal pressure during phase change. Therefore, the open pulsating heat pipe is a suitable device to move fluids if the heat source such as waste heat exists. Many numerical studies have not been sufficiently conducted on the open pulsating heat pipe. In this study, the numerical analysis of the open pulsating heat pipe is performed according to the length of the condenser section. The OpenFOAM software is used to obtain the thrust and the flow visualization for the open pulsating heat pipe.

Numerical Analysis of Ship's Propulsion Mechanism of Two-Stage Weis-Fogh Type by Discrete Vortex Method

  • 노기덕;한수환
    • Journal of Mechanical Science and Technology
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    • 제15권11호
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    • pp.1548-1554
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    • 2001
  • Flow patterns and dynamic properties of two-stage Weis-Fogh type ship propulsion mechanism are studied by a discrete vortex method. To study mutual interference between two wings, two cases are con sidered - wing motions with the same and reverse phases. The predicted flow patterns correspond to the available flow visualization results. Time histories of thrust and drag coefficients are also calculated, and the interference between the two wings are numerically clarified.

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반대방향 충돌제트에 의한 원형 챔버 내 혼합거동에 대한 전산가시화 (Numerical visualization of mixing in a circular chamber by two opposite impinging jets)

  • 하미드 카바시안;김영우;이인범;한범정;정용채;김경천
    • 한국가시화정보학회지
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    • 제14권3호
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    • pp.32-37
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    • 2016
  • In this study, the mixing process of two distinct flow is numerically investigated. Two flow with different physical properties (resin and hardener) are mixed through the opposing mixing jets. At a high pressure mixing process, the high speed flow is provided by two in-line nozzles. In the case of numerical modeling, Reynolds-Averaged Navier-Stokes Equations (RANS) is conducted to model the flow pattern inside the chamber. Additionally, SST k-omega turbulence model is selected to predict the kinetic energy of flow in impingement zone. The results show that mixing of two distinct flows would be efficient if the velocity of jet is high enough and nozzle diameter is a predominant parameter. Also, this velocity would create higher shear stress between two distinct flows which increases the mixing quality as well as strength of formed vortices. Eventually, the histogram of concentration fraction of resin is examined in order to show the quality of mixing and the range of concentration fractions in the output of chamber.

표면 장력 효과를 고려한 마이크로 채널 충전과정 연구 (Study of Micro-channel Filling Flow Including Surface Tension Effects)

  • 김동성;이광철;권태헌;이승섭
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2001년도 춘계학술대회논문집C
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    • pp.47-52
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    • 2001
  • Micro-injection molding and microfluidic devices with the help of MEMS technologies including the LIGA process are expected to play important roles in. micro-system industries, in particular the bioapplication industry, in the near future. Understanding fluid flows in micro-channels is important since micro-channels are typical geometry in various microfluidic devices and mold inserts for micro-injection molding. In the present study, both experimental and numerical studies have been carried out to understand the detailed flow phenomena in micro-channel filling process. Three sets of micro-channels of different thickness were fabricated and a flow visualization system was also developed to observe the filling flow into the micro-channels. Experimental flow observations were extensively made to find the effects of channel width and thickness, and effects of surface tension and volume flow rate and so on. And a numerical analysis system has been developed to simulate the filling flow into micro-channels with the surface tension effect taken into account. Discussed are the flow visualization experimental observations along with the predictability of the numerical analysis system.

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비스플라인 부피에 기초한 유동 가시화 모델 (Flow Visualization Model Based on B-spline Volume)

  • 박상근;이건우
    • 한국CDE학회논문집
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    • 제2권1호
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    • pp.11-18
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    • 1997
  • Scientific volume visualization addresses the representation, manipulation, and rendering of volumetric data sets, providing mechanisms for looking closely into structures and understanding their complexity and dynamics. In the past several years, a tremendous amount of research and development has been directed toward algorithms and data modeling methods for a scientific data visualization. But there has been very little work on developing a mathematical volume model that feeds this visualization. Especially, in flow visualization, the volume model has long been required as a guidance to display the very large amounts of data resulting from numerical simulations. In this paper, we focus on the mathematical representation of volumetric data sets and the method of extracting meaningful information from the derived volume model. For this purpose, a B-spline volume is extended to a high dimensional trivariate model which is called as a flow visualization model in this paper. Two three-dimensional examples are presented to demonstrate the capabilities of this model.

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PIV 가시화에 의한 합류덕트에서의 유동특성 (Flow Characteristics for PIV Visualization at Junction Duct)

  • 김명관;권오붕;배대석
    • 동력기계공학회지
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    • 제9권4호
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    • pp.45-50
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    • 2005
  • Characteristics of flows at T-junction duct with and without orifices are investigated in this paper. Experiments and PIV visualization were carried out for several flow rates. Two-dimensional PIV experimental apparatus was decided by numerical analysis. PIV visualization was also coded to visualize flow fields at junctions for two-dimensional case. For the PIV visualization system, Grey-Level Cross-Correlation particle tracking algorithm was used to calculate the flow fields. Vinyl chloride polymer particles of $100{\sim}150{\mu}m$ of diameter are used in this visualization. The PIV visualization results showed relatively good agreement with Experimental data.

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프링-크래핑 날개의 주기적 운동에 관한 수치적 흐름 가시화 (Numerical Flow Visualization of Cyclic Motion of a Fling-Clapping Wing)

  • 장조원;손명환
    • 대한기계학회논문집B
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    • 제28권12호
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    • pp.1511-1520
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    • 2004
  • A flow visualization of the two-dimensional rigid fling-clap motions of the flat-plate wing are performed to gain knowledge of butterfly mechanisms that might be employed by butterflies during flight. In this numerical visualization, the time-dependent Navier-Stokes equations are solved for cyclic fling and clap types of wing motion. The separation vortex pair that is developed in the fling phase of the cyclic fling and clap motion is observed to be stronger than those of the fling followed by clap and pause motion(1st cycle motion). This stronger separation vortex pair in the fling phase is attributable to the separation vortex pair of the outside space developed in the clap phase as it moves into the opening in the following fling phase. Accordingly, higher lift and power expenditure coefficients in the fling after clap phase is caused by the stronger separation vortex pair.