• Title/Summary/Keyword: Fluids Interaction

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Helium-Air Exchange Flow with Fluids Interaction (유체간섭을 동반하는 헬륨과 공기의 치환류)

  • T.I. Kang
    • Journal of Advanced Marine Engineering and Technology
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    • v.21 no.4
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    • pp.372-380
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    • 1997
  • This paper describes experimental investigations of helium-air exchange flows through parti¬tioned opening and two-opening. Such exchange flows may occur following rupture accident of stand pipe in high temperature gas cooled reactor. A test vessel with the two types of small open¬ing on top of test cylinder is used for experiments. An estimation method of mass increment is developed and applied to measure the exchange flow rate. A technique of flow visualization by Mach-Zehnder interferometer is provided to recognize the exchange flows. In the case of exchange flow through the partitioned opening, flow passages of upward flow of the helium and downward flow of the air within the opening are separated by vertical partition, and the two flows interact out of entrance and exit of the opening. Therefore, an experiment of the exchange flow through two-opening is made to investigate effect of the fluids interaction of the partitioned opening sys¬tem. As a result of comparison of the exchange flow rates between the two types of the opening system, it is found that the exchange flow rate of the two-opening system is larger than that of the partitioned opening system due to absence of the effect of fluids interaction. Finally, the fluids interaction between the upward and downward flows through the partitioned opening is found to be an important factor on the helium-air exchange flow.

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Hydrodynamic interaction between two cylinders in planar shear flow of viscoelastic fluid

  • Jung, Hyun-Wook;Daejin Won;Kim, Chongyoup
    • Korea-Australia Rheology Journal
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    • v.14 no.4
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    • pp.203-207
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    • 2002
  • Particle-particle interaction is of great importance in the study of suspension rheology. In this research we have investigated the hydrodynamic interaction between two identical cylinders in viscoelastic fluids numerically as a model problem for the study of viscoelastic suspension. We confine two neutrally buoyant cylinders between two parallel plates and impose a shear flow. We determine the migration velocity of two cylinders. The result shows that cylinders move toward or away from each other depending upon the initial distance between them and that there is an equilibrium distance between two cylinders in viscoelastic fluids regardless of the initial distance. In the case of Newtonian fluid, there is no relative movement as expected. The results partly explain the chaining phenomena of spherical particles in shear flows of viscoelastic fluids.

DYNAMICAL MAGNETIC PROPERTIES OF IRON-NITRIDE MAGNETIC FLUIDS

  • Mamiya, H.;Nakatani, I.
    • Journal of the Korean Magnetics Society
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    • v.5 no.5
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    • pp.815-818
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    • 1995
  • Ac susceptibility of iron-nitride magnetic fluids with various particle number densities was measured. Therelaxation time increases rapidly as the temperature decreases or the inter-particle interaction increases. The analysis of the data suggests that the activation energy is proportional to ${(k_{B}T/J_{typ})}^{\alpha}$ with $\alpha$~-0.24 in the lower temperature range in which the thermal energy is comparable to the magnetic dipole interaction.

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2-D Inviscid Analysis of Flow in One Stage of Axial Compressor (1단 축류압축기 내부 유동의 2차원 비점성 해석)

  • Kim HyunIl;Park JunYoung;Baek JeHyun;Jung HeeTaek
    • Journal of computational fluids engineering
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    • v.5 no.2
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    • pp.38-46
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    • 2000
  • It has been indicated that the rotor/stator interaction has distinct causes of unsteadiness, such as the viscous vortex shedding, wake/stator interaction and potential rotor/stator interaction. In this paper, the mechanism of unsteady potential interaction in one stage axial compressor is numerically investigated for blade row ratio 1:1 and 2:3 at design point and for blade row ratio 2:3 at off-design point in two-dimensional view point. The numerical technique used is the upwind scheme of Van-Leer's Flux Vector Splitting(FVS) and Cubic spline interpolation is applied on zonal interface. In this study the flow unsteadiness due to potential interaction are found to be larger in blade row ratio 2:3 than in 1:1. The total pressure rise in blade row ratio 2:3 is closer to the real value in design point than that in 1:1. The change of unsteady pressure amplitude according to the variation of stator exit pressure is very small.

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A Flow/structure Interaction Analysis for the Design of Medical CSF-Flow Control Valve (의료용 CSF 제어 밸브 설계를 위한 유동/구조 상호작용 해석)

  • Won C. S.;Hur N.;Lee C. S.
    • Journal of computational fluids engineering
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    • v.6 no.1
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    • pp.40-46
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    • 2001
  • Pressure-flow control characteristics of a commercially available cerebrospinal flow(CSF) control shunt valve was studied using flow/structure interaction analyses. Pre-stress of the valve diaphragm(membrane) was accounted for the simulation of an actual valve. The present results were in good agreement with the valve specification listed in the commercially available CSF control valve. The flow/structure interaction analysis of the present study can be effectively used to design a variety of CSF control shunt valves.

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NUMERICAL STUDY ON DPS THRUSTER-HULL INTERACTION WITH DIFFERENT AXIS TILTING ANGLE (축기울기에 따른 DPS 스러스터와 선체의 상호간섭 수치해석)

  • Jin, D.-H.;Lee, S.-W.
    • Journal of computational fluids engineering
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    • v.21 no.1
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    • pp.72-77
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    • 2016
  • In this study, effects of thurster axis tilting angle on the thruster-hull interaction and propulsion performance in a dynamic positioning system of offshore plant are numerically investigated. Straight and 7-degree tilted downward thruster models as a form of ducted propeller are considered. For numerical simulations, Reynolds averaged Navier-Stokes equations with SST turbulence model are solved by using STAR-CCM+. Results show that thruster-hull interaction is reduced in 7-degree tilted thruster model with lower vortex strength between thruster and hull bottom, although the propulsion performance does not have noticeable difference in a bollard condition.

Microstructure and shear modulus in concentrated dispersions of bidisperse charged spherical colloids

  • Chun, Myung-Suk;Lee, Sangwoo;Lee, Tae-Seok;Cho, Jae-Seol
    • Korea-Australia Rheology Journal
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    • v.16 no.1
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    • pp.17-26
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    • 2004
  • We examine rigorous computations on microstructural as well as rheological properties of concentrated dispersions of bidisperse colloids. The NVT Monte Carlo simulation is applied to obtain the radial distribution function for the concentrated system. The long-range electrostatic interactions between dissimilar spherical colloids are determined using the singularity method, which provides explicit solutions to the linearized electrostatic field. The increasing trend of osmotic pressure with increasing total particle concentration is reduced as the concentration ratio between large and small particles is increased. From the estimation of total structure factor, we observe the strong correlations developed between dissimilar spheres. As the particle concentration increases at a given ionic strength, the magnitude of the first peak in structure factors increases and also moves to higher wave number values. The increase of electrostatic interaction between same charged particles caused by the Debye screening effect provides an increase in both the osmotic pressure and the shear modulus. The higher volume fraction ratio providing larger interparticle spacing yields decreasing high frequency limit of the shear modulus, due to decreasing the particle interaction energy.

THE NUMERICAL STUDY ON THE SUPERSONIC INLET FLOW FIELD WITH A BUMP (Bump가 있는 초음속 흡입구 유동장의 수치적 연구)

  • Kim S. D.;Song D. J.
    • Journal of computational fluids engineering
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    • v.10 no.3 s.30
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    • pp.19-26
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    • 2005
  • The purpose of this paper is the study on the characteristics of an inlet system with shock/boundary layer interactions by using various types of bumps which are substituted for the conventional bleeding system in supersonic inlet. in this study a comprehensive numerical analysis has been performed to understand the three-dimensional flow field including shock/boundary layer interaction and growth of turbulent boundary layer that might occur around a three-dimensional bump in a supersonic inlet. The characteristics of boundary layer seen in the current numerical simulations indicate the potential capability of a three-dimensional bump to control shock/boundary layer interaction in supersonic inlets.

Prediction of Deformation of an Oil-fence by using Fluid$\cdot$Structure Interaction Method (유체$\cdot$구조물 상호 작용 기법을 이용한 오일 펜스의 변형 예측)

  • Kim T. G.;Kim W.;Hur N.
    • Journal of computational fluids engineering
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    • v.5 no.3
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    • pp.16-22
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    • 2000
  • In the present study a method of computing fluid-structure interaction is presented to simulate the deformation shape of an oil fence which is used to contain or to divert the split oil in sea water. The computation is performed by taking into account of the force and moment balance in each computational element of the oil fence. The forces and moments acting on each element of the structure is computed from the flow analysis, which in turn is used to predict deformed shape of the structure until the procedure converges. The flexibility of the oil fence was also considered in the analysis. It is shown from the present study that the predicted deformed shapes agree quite well with the available experiment data.

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