• 제목/요약/키워드: air-particle flow

검색결과 394건 처리시간 0.022초

PIV기법을 이용한 룸에어컨 주변 유동 분포 해석 (Analysis of Flow Distribution around Room Air Conditioner Using PIV Technique)

  • 이아미;한규일;김동원;라선욱;주재만;고한서
    • 한국가시화정보학회:학술대회논문집
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    • 한국가시화정보학회 2006년도 추계학술대회 논문집
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    • pp.131-134
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    • 2006
  • Whole flow fields of a room air conditioner (RAC) have been visualized by a Particle Image Velocimetry (PIV) technique to analyze the flow structure by various inlet and outlet angles, and to control an eccentric vortex which affects an efficiency and noise of the RAC. A test model with 5 stages of a cross flow fan has been manufactured and a transparent acryl has been installed at the side of the test model for the PIV experiment. The inlet and outlet flows and the flow inside the cross flow fan have been analyzed by varying the inlet grill angles and outlet blade angles. The movement of the eccentric vortex has been investigated experimentally by developing the measurement technique for the inner flow field of the cross flow fan, and the relationship between the control of the eccentric vortex and the inlet and outlet angles has been confirmed in this study.

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공기흐름을 고려한 수리-역학적 연동모델에 의한 불포화 토사사면의 안정해석 (Stability Analysis of Unsaturated Soil Slope by Coupled Hydro-mechanical Model Considering Air Flow)

  • 조성은
    • 한국지반공학회논문집
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    • 제32권1호
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    • pp.19-33
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    • 2016
  • 강우의 침투가 사면안정에 미치는 영향을 평가하기 위해 강우의 침투해석을 수행하고 그 결과를 한계평형해석에 적용하는 안정해석 절차가 널리 사용되고 있으나 지반은 흙 입자, 물과 공기로 이루어진 3상의 물질이므로 사면을 통한 강우의 침투를 엄밀하게 해석하기 위해서는 물, 공기의 흐름과 흙의 응력-변형거동이 완전 연관된(fully coupled) 식을 고려해야 한다. 본 연구에서는 공기와 물의 흐름이 사면의 역학적 안정에 미치는 영향을 연구하기 위하여 우리나라에 널리 분포하는 풍화잔류토 사면에 대하여 3상이 연동된 흐름해석을 수행하였다. 강우침투가 사면안정에 미치는 영향을 평가하기 위하여 강도감소법에 의한 사면 안정해석을 수행하였다. 해석결과에 의하면 침투하는 강우가 공기를 밀어내 공기의 흐름이 발생하고 공기압이 증가하였다. 이러한 간극에서의 물과 공기의 상호작용은 사면의 응력-변형거동에 영향을 미쳐 공기의 흐름을 고려하지 않은 흙 입자-물의 연관해석의 결과와는 다른 사면안정 거동을 보였다.

The Characteristics of Pulverized Coal Combustion in the Two Stage Cyclone Combustor

  • Joo, Nahm-Roh;Kim, Ho-Young;Chung, Jin-Taek;Park, Sang-Il
    • Journal of Mechanical Science and Technology
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    • 제16권9호
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    • pp.1112-1120
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    • 2002
  • Numerical investigations on air staging and fuel staging were carried out with a newly designed coaxial cyclone combustor, which uses the method of two stage coal combustion composed of pre-combustor and main combustor. The pre-combustor with a high air/fuel ratio is designed to supply gas at high temperature to the main combustor. To avoid local high temperature region in this process, secondary air is injected in the downstream. Together with the burned gas supplied from the pre-combustor and the preheated air directly injected into main combustor, coals supplied through the main burner react rapidly at a low air/fuel ratio. Strong swirling motion of cyclone combustor keeps the wall temperature high, which makes slagging combustion possible. Alaska, US coal is used for calculations. Predictions were made for various coal flow rates in the main combustor for fuel staging and for the various flow rate of secondary air in the pre-combustor for air staging. In-scattering angles are also chosen as a variable to increase residence times of coal particles. Temperature fields and particle trajectories for various conditions are described. Predicted temperature variations at the wall of the combustor are compared with corresponding experimental data and show a similar trend. The in-scattering angle of 20° is recommended to increase the combustion efficiency in the main chamber.

감쇠탱크 설계를 위한 체류시간 계산 방법에 관한 연구 (A Study of Residence Time Calculation Methods in Decay Tank Design)

  • 정민규;서경우;김성훈
    • 설비공학논문집
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    • 제29권5호
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    • pp.220-230
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    • 2017
  • In this study we apply and compare a variety of numerical methods for calculating residence time distribution in decay tanks, a major design component in the for reducing N-16 radioactivity. Our research group has used a streamlined method using user-defined particle numbers. However, this streamlined method has several problems, including low exiting particle ratios, particle diminishing, and unphysical time distribution, among others. We utilize three numerical methods to establish residence time and time distribution (streamlined, discrete phase method [DPM], and user defined scalar [UDS]) and subsequently compare the averaged results of each. The three tests demonstrate the flow features within the decay tanks, which are then numerically simulated to enable comparison. We conclude that although each simulation predicts similar time averages, the UDS methodology provides a smoother time distribution and tracer contour plots at specific times.

횡방향 유속 변화에 따른 고압 가솔린 스월 인젝터의 분무특성 (Spray Characteristics of High Pressure Gasoline Swirl Injector with Various Cross-flow Speeds)

  • 최재준;이용석;최욱;배충식
    • 한국자동차공학회논문집
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    • 제13권1호
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    • pp.1-8
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    • 2005
  • The spray prepared for direct fuel injection into cylinder is of great importance in a DISI(Direct Injection Spark Ignition) engine. The interaction between air flow and fuel spray was investigated in a steady flow system embodied in a wind tunnel to simulate the variety of in-cylinder flow conditions in the DISI engine. The Mie-scattering images presented the macroscopic view of the liquid spray fields interacting with cross-flow Particle sizes of fuel droplets were measured with phase Doppler anemometer(PDA) system. A faster cross-flow field made SMD larger and $D_10$ smaller. The atomization and evaporation processes with a DISI injector were observed and consequently utilized to construct the database on the spray and fuel-air mixing mechanism as a function of the flow characteristics.

다공 디젤분무의 액적-공기 상대속도 측정에 관한 실험적 연구 (An Experimental Study on the Measurement of the Droplet-Air Relative Velocity in the Multi-hole Diesel Spray)

  • 권명훈;신형민;이지근;강신재;노병준
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2000년도 춘계학술대회논문집B
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    • pp.801-806
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    • 2000
  • This experimental study is to investigate the intermittent spray characteristics of a multi-hole nozzle in a heavy-duty DI diesel engine. Multi 8 hole$(d_n=0.25mm)$, Multi 3 hole$(d_n=0.42)$ and Sing hole nozzle$(d_n=0.25mm)$ were used in this experiment. By using the 2-D PDPA(phase Doppler particle analyzer), the droplet diameter and the velocity of a diesel spray injected intermittently from the multi and the single-hole nozzle into a still ambient were measured. In order to calculate the mean values such as mean velocity, SMD, AMD etc. and to analyze the intermittent characteristics, the time-window of 0.15ms were applied. In the spray, the small droplet$(D<10{\mu}m)$ was regarded as an air flow, and the correlation between the fuel droplet$(10{\mu}m and the air (low was examined. The normalized axial droplet-air relative velocity of the 8 hole, the 3 hole and the single hole nozzle was evaluated as 0.081, 0.067, 0.06 and in case of the radial droplet-air relative velocity, the normalized. value is 0.014, 0.013 and 0.008 respectively.

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전산유체 기법을 이용한 용존공기부상법에서의 접촉도 조건변화에 따른 충돌효율평가 (Collision Efficiency Estimation in the DAF Contact Zone using Computational Fluid Dynamics)

  • 김성훈;유제선;박희경
    • 상하수도학회지
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    • 제18권2호
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    • pp.201-207
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    • 2004
  • Dissolved air flotation (DAF) is a solid-liquid separation process that uses fine rising bubbles to remove particles in water. Most of particle-bubble collision occurs in the DAF contact zone. This initial contact considered by the researchers to play a important role for DAF performance. It is hard to make up conceptual model through simple mass balance for estimating collision efficiency in the contact zone because coupled behavior of the solid-liquid-gas phase in DAF system is 90 complicate. In this study, 2-phase(gas-liquid) flow equations for the conservation of mass, momentum and turbulence quantities were solved using an Eulerian-Eulerian approach based on the assumption that very small particle is applied in the DAF system. For the modeling of turbulent 2-phase flow in the reactor, the standard $k-{\varepsilon}$ mode I(liquid phase) and zero-equation(gas phase) were used in CFD code because it is widely accepted and the coefficients for the model are well established. Particle-bubble collision efficiency was calculated using predicted turbulent energy dissipation rate and gas volume fraction. As the result of this study, the authors concluded that bubble size and recycle ratio play important role for flow pattern change in the reactor. Predicted collision efficiency using CFD showed good agreement with measured removal efficiency in the contact zone. Also, simulation results indicated that collision efficiency at 15% recycle ratio is higher than that of 10% and showed increasing tendency of the collision efficiency according to the decrease of the bubble size.

AN OPTIMUM DESIGN STUDY OF INTERLACING NOZZLE BY ANALYZING FLUID FLOW INSIDE INTERLACING NOZZLES

  • Juraeva Makhsuda;Ryu Kyung Jin;Kim Sang Dug;Song Dong Joo
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2005년도 추계 학술대회논문집
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    • pp.93-97
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    • 2005
  • Air interlacing serves to protect the yarn against damage, strengthens inter-filament compactness or cohesion, and ensures fabric consistency. The air interlacing nozzle is used to introduce intermittent nips to a filament yarn so as to improve its performance in textile processing. This study investigates the effect of interlacing nozzle geometry on the interlacing process. The geometries of interlacing nozzles with multiple air inlets located across the width of a yarn channels are investigated. The basic interlacing nozzle is the yarn channel, with a perpendicular single air inlet in the middle. The yarn channel shapes are cross sections with semicircular or rectangular shapes. This paper presents three doubled sub air inlets with main air inlet and one of them is slightly inclined doubled sub air inlets with main air inlet. The compressed air coming out from the inlet hits the opposing wall of the yarn channel, divides into two branches, flows trough the top side of yarn channel, joins with the compressed air coming out from the sub air inlet and then creates two free jets at both ends of the yarn channel. The compressed air moves in the shape of two opposing directional vortices. The CFD-FASTRAN was used to perform steady simulations of impinging jet flow inside of the interlace nozzles. The vortical structure and the flow pattern such as pressure contour, particle traces, velocity vector plots inside of interlace nozzle geometry are discussed in this paper.

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평등전계에서 도전성 구형 입자의 운동 (Motion of Conductive Spherical Particle under Uniform Electric Field)

  • 임헌찬
    • 조명전기설비학회논문지
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    • 제25권8호
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    • pp.39-47
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    • 2011
  • The motion of a conductive spherical particle under uniform electric field is investigated in order to find a suitable method for removing the conducting solid impurities contained in liquid plastic. When the positive dc voltage applied to the upper electrode, the vertical up-and-down motion of a charged particle by electrostatic force is observed by a charge-coupled device (CCD) camera or a high-speed video camera. The experimental data of the static threshold voltage by which the particle starts to move toward the counter electrode in air or silicone oil are in good agreement with theoretical value. When the applied voltage is larger than the static threshold voltage, the particle motion pattern in silicone oil consists of four stages: upward motion, stopping at the upper electrode, downward motion and stopping at the lower electrode. The stopping motion on the electrode is thought to be caused by the liquid flow accompanied by the particle motion. The particle charge calculated by integrating the pulse current, which is generated by the charge exchange between the electrode and the particle, is approximately 0.1~0.25 times of the theoretical value. This study is expected to help understand the electric properties of microparticles in oil circuit breaker (OCB) and oil transformer and improve their performance and longevity.

PIV에 의한 수중램제트추진의 기본특성에 관한 연구 (A Study on Fundamental Characteristics of Underwater Ram-Jet Propulsion by PIV)

  • 양창조;김춘식;최민선;김진구;이영호
    • Journal of Advanced Marine Engineering and Technology
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    • 제24권3호
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    • pp.36-42
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    • 2000
  • A fundamental experimental study for an alternative proposal to super-speed craft propulsion system called underwater ram-jet propulsion by high pressure air ejection as driving force was investigated. For basic study of the effects of ram-jet propulsion performance, a simple underwater ram-jet flow field was established and PIV(Particle Image Velocimetry) method was adopted to analyse the jet-induced flow appearing at ram intake, mixing chamber and nozzle. Some flow dynamics relating to the high-speed ram-jet effect were discussed for the basic understanding of the its propulsion principle.

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