• 제목/요약/키워드: 2상 유동

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Two-phase Pressure Drop in a Horizontal Rectangular Microchannel (수평 사각 마이크로채널 내에서의 2상 유동 압력강하)

  • Huh, Cheol;Kim, Moo-Hwan
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.30 no.11 s.254
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    • pp.1035-1042
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    • 2006
  • An experimental investigation was performed to study two-phase pressure drop of deionized water in a microchannel. Measurement and evaluation of two-phase frictional pressure gradient were carried out using a single horizontal rectangular microchanne1 having a hydraulic diameter of $100{\mu}m$. Tests were performed for mass fluxes of 90, 169, and 267 $kg/m^2$s and heat fluxes of 200-700 $kW/m^2$. Test results showed that the measured two-phase frictional pressure gradient increased with the mass flux and vapor quality. Most macro-channel correlations of two-phase frictional pressure gradient did not provide reliable predictions except under certain limited conditions.

Fluid-elastic Instability in a Tube Array Subjected to Two-Phase Cross Flow (2 상 횡 유동장에 놓인 관군의 유체탄성불안정성)

  • Sim, Woo-Gun;Park, Mi-Yeon
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.33 no.2
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    • pp.124-132
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    • 2009
  • Experiments have been performed to investigate fluid-elastic instability of tube bundles, subjected to twophase cross flow. Fluid-elastic is the most important vibration excitation mechanism for heat exchanger tube bundles subjected to the cross flow. The test section consists of cantilevered flexible cylinder(s) and rigid cylinders of normal square array. From a practical design point of view, fluid-elastic instability may be expressed simply in terms of dimensionless flow velocity and dimensionless mass-damping parameter. For dynamic instability of cylinder rows, added mass, damping and the threshold flow velocity are evaluated. The Fluid-elastic instability coefficient is calculated and then compared to existing results given for tube bundles in normal square array.

열유동 상분리막의 구조연구

  • ;;Douglass, K. Lolyd
    • Membrane Journal
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    • v.1 no.1
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    • pp.13-23
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    • 1991
  • 열유도 상분리법을 이용하여 제조되는 분리막의 구조 변화를 열역학 및 속도론적 관점에서 고찰하였다. Polypropylene과 희석제로서 n-alkanes, n-fatty acids, n,n-bis(2-hydroxyethyl) tallowamine을 model system으로 하였다. 고분자/희석제 system의 상변화의 종류에 따라 다양한 형태의 분리막구조가 얻어졌다. 분리막의 구조에 영향을 미치는 변수로서 고분자/희석제간의 interaction parameter, 희석제의 분자 크기, 용액의 조성, 냉각 조건, 희석제의 결정화 온도 등이며, 각 변수의 역할을 전자현미경을 사용하여 규명하였다. 열유동 상분리법에 의하여 제조된 분리막은 inter-spherulitic 및 intra-spherulitic pore의 이중 구조로 이루어짐을 확인하였다.

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Accurate and Robust Computations of Gas-Liquid Two-Phase Flows Part 2: Preconditioned Two-Phase Schemes for All Speeds (액체-기체 2상 유동장의 정확하고 강건한 해석 Part 2: 전 마하수 영역 해석을 위한 예조건화)

  • Ihm, Seung-Won;Kim, Chong-Am
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.37 no.1
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    • pp.17-27
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    • 2009
  • Two-phase RoeM and AUSMPW+ schemes are preconditioned for the simulation of all Mach number flows, which are generally of interest for many gas-liquid two-phase application problems, because of large speed of sound in liquid region and low speed of sound in mixture or gas region. Conventional characteristic based schemes lose their accuracy or robustness in low Mach number flows, because their numerical dissipation terms are scaled by speed of sound, which is too large compared with local velocity magnitude in a low Mach region. All speed versions of RoeM and AUSMPW+ reflect the eigenvalues of the preconditioned governing system, which have the same order of magnitude even in low Mach number region. From the asymptotic analysis, it is observed that the discretized system by the developed schemes is consistent with the continuum system in the incompressible limit. The numerical results show the accurate and robust behavior of the proposed shcemes for all speed two-phase flows.

Application of Lumley's Drag Reduction Model to Two-Phase Gas-Particle Flow in a Pipe(I) - Mechanism of Momentum Transfer- (고체분말이 부상하는 2상 난류 수직관 유동에 대한 Lumley의 저항감소 모델의 적용(I) - 운동량 전달 기구)

  • 한기수;정명균;성형진
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.13 no.6
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    • pp.1301-1309
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    • 1989
  • 본 연구의 목적은 Lumley의 저항감소 모델을 사용하여 여러 부하도하에서 부유유동의 유동 특성을 관찰하는 것으로, 특히 저항감소가 일어날 때와 일어나지 않을 때의 유동특성을 알아 보고자 한다.

Size and Rising Velocity of Liquid Drops in Liquid-Liquid Fluidized-Bed Extractors (유동층 액-액 추출기에서 액적의 크기 및 상승속도)

  • Jung, Sung-Hyun;Kim, Jae-Han;Kang, Tae-Gyu;Kang, Yong;Kim, Sang Done
    • Applied Chemistry for Engineering
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    • v.16 no.1
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    • pp.34-38
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    • 2005
  • Characteristics of size, rising velocity and distribution of liquid drops have been investigated in a immiscible liquid-liquid fluidized-bed whose diameter was 0.102 m and 2.5 m in height. Effects of velocities of dispersed (0~0.04 m/s) and continuous (0.02~0.14 m/s) liquid phases and fluidized particle size (1, 2.1, 3 or 6 mm) on the liquid drop properties in the extractor have been determined. The resultant flow behavior of liquid drops became more complicated with increasing the velocity of dispersed or continuous liquid phase. The resultant flow behavior of liquid complicated with increasing the velocity of dispersed or continuous liquid phase. The resultant flow behavior of liquid drops depended strongly upon the drop size and its distribution. The drop size increased with increasing dispersed phase velocity, but decreased with increasing particle size. However, the size of liquid drop exhibited a local maximum with increasing continuous liquid velocity. The size and rising velocity of liquid drops have been well correlated in terms of operating parameters.

지하유류저장시설 주변의 단열암반 내 지하수유동체계 해석

  • Jo Seong-Il;Kim Cheon-Su;Bae Dae-Seok;Kim Gyeong-Su;Park Gyeong-U;Song Mu-Yeong
    • Proceedings of the Korean Society of Soil and Groundwater Environment Conference
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    • 2005.04a
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    • pp.292-295
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    • 2005
  • 본 연구는 지하유류저장공동 굴착 시 비교적 정밀하게 해석된 단열체계 및 수리인자를 토대로 투수성구조영역과 수리암반영역으로 세분화하여 연구지역의 불규칙하고 복잡한 지하수유동체계를 해석해 보고자 하였다. FZ-2 구조대와 인접한 수리암반영역 Domain-A와 B는 Domain-C와 D에 비해 수평수벽공의 초기압이 최대 약 $15kg/cm^2$정도 높으며, 상 하부의 수리적 연결성이 양호하여 지하공동굴착 시 상 하부의 수위차가 크지 않고 지하수 함양량은 약 $35{\sim}50mm/year$의 범위를 보인다. 또한 공동굴착 시 투수성 단열과의 교차에 의한 수위강하에 민감한 반응을 보이며 상 하부의 수위강하양상이 유사한 특성을 나타낸다. 반면, FZ-1 구조대와 인접한 Domain-C와 D는 지하공동 부근의 수리전도도가 각각 $7{\times}10^{-10},\;2{\times}10^{-9}m/sec$로 Domain-A와 B에 비해 최대 약 6배정도 낮고, 상 하부의 수리적 연결성이 양호하지 않기 때문에 공동굴착 전 이중수위측정시설 설치 시 계측된 상 하부의 수위차는 최대 약 120 m로 매우 크다. 그리고 상부의 지하수는 하부의 낮은 수리전도도로 인하여 수직방향보다 수평방향으로의 유동이 우세하며 공동굴착 시 수위변화는 크지 않고 함양량은 $10{\sim}15mm/year$의 범위를 나타낸다.

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Numerical Simulation Study on Gas-Particle Two-Phase Jets in a Crossflow (I) -Two-Phase Jet Trajectory and Momentum Transfer Mechanism- (고체입자가 부상된 자유 횡분류 유동에 대한 전산모사 연구 (I) -2상 분류궤적과 운동량 전달기구-)

  • 한기수;정명균
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.15 no.1
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    • pp.252-261
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    • 1991
  • A particle trajectory model to simulate two-phase particle-laden crossjets into two-dimensional horizontal free stream has been developed to study the variations of the jet trajectories and velocity variations of the gaseous and the particulate phases. The following conclusions may be drawn from the predicted results, which are in agreement with experimental observations. The penetration of the two-phase jet in a crossflow is greater than that of the single-phase jet. The penetration of particles into the free stream increases with increasing particle size, solids-gas loading ratio and carrier gas to free stream velocity ratio at the jet exit. When the particle size is large, the solid particles separate from the carrier gas , while the particles are completely suspended in the carrier gas for the case of small size particles. As the particle to carrier gas velocity ratio at the jet exit is less than unity, the particles in the vicinity of the jet exit are accelerated by the carrier gas. As the injection angle is increased, the difference of the particle trajectory from that of the pure gas becomes larger. Therefore, it can be concluded that the velocities and trajectories of the particle-laden jets in a crossflow change depending on the solids-gas loading ratio, particle size, carrier gas to free stream velocity ratio and particle to gas velocity ratio at the jet exit.

전기임피던스 영상에 의한 2상유동에서의 기포분포의 가시화

  • Cho, Kyung-Ho;Kim, Sin;Lee, Yun-Jun
    • Proceedings of the Korean Nuclear Society Conference
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    • 1998.05a
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    • pp.457-462
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    • 1998
  • 유동장에서의 기포거동 정보의 중요성 때문에 이를 정확히 측정하기 위한 실험방법이 여러 가지로 발전해 왔지만 아직까지도 기포분포에 대한 정확한 정보 추출에는 도달하지 못하고 있다. 본 연구에서는 원래 의공학분야에서 새로운 tomography 기술로 연구되고 있는 EIT(Electrical Impedance Tomography) 기술을 2상유동에서의 기포분포 측정방법 개발에 적용하기 위한 기초연구와 기포분포 가시화를 위한 전산실험을 수행하였다. 기포분포 가시화를 위해서는 EIT inverse problem solver로 많이 사용되는 iNR(improved Newton-Raphson) 계열의 EIT 염상복원 프로그램을 본 연구진이 유전알고리즘(Genetic Algorithm)과 fuzzy-based mesh grouping 방법을 추가하여 개선한 영상복원프로그램을 사용하였다. 전산실험 결과 본 영상복원프로그램으로는 12$\times$12의 분해능으로 모사되는 기포분포를 저항률 오차한도 $\pm$1%의 신뢰도로 PC상에서 복원이 가능함을 확인하였다.

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A Numerical Validation for Incompressible Two-phase Flow using CLSVOF and Artificial Compressibility Methods (CLSVOF과 가상압축성 기법을 이용한 비압축성 2상 유동 수치해석 검증 연구)

  • Yoo, Young-Lin;Choi, Jeong-Yeol;Sung, Hong-Gye
    • Journal of the Korean Society of Propulsion Engineers
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    • v.21 no.5
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    • pp.71-79
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    • 2017
  • A numerical analysis of the liquid-gas two-phase flows has been conducted. The incompressible equations of the two-phase flows were solved by the artificial compressibility method with the CLSVOF interface capturing method. To analyze the grid dependency of CLSVOF, a numerical analysis of Zalesak's disk and three-dimensional liquid deformation problem were carried out, and the reconstruction of deformation was investigated. The Rayleigh-Taylor instability was numerically analyzed by applying the equations of incompressible two-phase flow, and the surface instability was observed.