• 제목/요약/키워드: Evaporating Liquid

검색결과 77건 처리시간 0.02초

Heat Transfer of an Evaporating Liquid on a Horizontal Plate

  • Joo, Sang-Woo;Park, Min-Soo;Kim, Min-Suk
    • Journal of Mechanical Science and Technology
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    • 제19권8호
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    • pp.1649-1661
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    • 2005
  • We consider. a horizontal static liquid layer on a planar solid boundary. The layer is evaporating when the plate is heated. Vapor recoil and thermo-capillary are discussed along with the effect of mass loss and vapor convection due to evaporating liquid and non-equilibrium thermodynamic effects. These coupled systems of equations are reduced to a single evolution equation for the local thickness of the liquid layer by using a long-wave asymptotics. The partial differential equation is solved numerically.

영광 3&4와 5&6호기에서 액체 방사성폐기물 처리방법의 비교 (The Comparison on Treatment Method of Liquid Radioactive Waste in Yonggwang #3&4 and #5&6)

  • Yeom, Yu-Seon;Kim, Soong-Pyung;Lee, Seung-Jin
    • 방사성폐기물학회지
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    • 제2권3호
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    • pp.219-230
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    • 2004
  • Most of the low-level liquid radioactive wastes generated from PWR plants are classified into high or low total suspended solid(HTDS or LTDS), and into radiochemical and radioactive laundry waste. Although the evaporation process has a high decontami- nation ability, it has several problems such as corrosion, foam, and congestion. A new liquid waste disposal process using the ion-exchange demineralizer(IED), instead of the current evaporation process, has been introduced into the Yonggwang NPP #5 and 6. These two methods have been compared to understand the differences in this study. Aspects compared here were the released radioactivity amount of the liquid radioactive wastes, the dose of off-site residents, the decontamination factor, and the amount of the solid radioactive wastes. The IED system is designed to discharge higher radioactivity about 20% than the evaporating system, and the actual radioactivity released from the evaporating and IED system were 0.473mCi and 1.098mCi, respectively. The radioactivity released from the IED was 2.32 times higher than that of the evaporating system. The dose of off-site residents was $2.97{\times}10^{-6}$mSv for the evaporating system, and $6.47{\times}10^{-6}$mSv for IED. The decontamination factor(DF) of the evaporator is, in most cases, far lower than the lower limits of detection(LLD) with the Ge-Li detector. Due to the low concentration of the liquid wastes collected from the liquid waste system, the decontamination factor of IED is very low. Since there is not enough data on the amount of solid radioactive wastes generated by the evaporation system, the comparison on these two systems has been conducted on the basis of the design, and the comparison result was that the evaporating system generated more wastes about 40% than IED.

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LIEF법을 이용한 증발 디젤 분무의 특성에 관한 연구 (A Study on the Characteristics of an Evaporating Diesel Spary Using LIEF Technique)

  • 김용래;김만식;조훈;민경덕
    • 한국분무공학회지
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    • 제7권3호
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    • pp.18-23
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    • 2002
  • An evaporating diesel spray of a common rail lnjector was visualized by LIEF technique. This technique makes it possible to separate the vapor and liquid phase images. The experiment was conducted in a constant volume vessel to make a high temperature and high pressure condition. Three images(vapor and liquid phase images from LIEF and a liquid phase image from Mie scattering) were taken simultaneously in one spray event. The major experimental parameters are the injection pressure and the ambient gas pressure. Also, a relative SMD distribution in a liquid phase was obtained by the ratio of the intensities of the fluorescence and the Mie scattering. The results show that the injection pressure and the ambient gas pressure have a close relation with the spray development and air-fuel muting process.

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정상 할로우 콘 분무와 환형 공기 제트의 상호작용에 관한 수치적 연구 (Numerical Investigation of a Steady Non-Evaporating Hollow-Cone Spray Interacting with an Annular Air Jet)

  • 김우태;허강열
    • 한국분무공학회지
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    • 제5권2호
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    • pp.43-52
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    • 2000
  • Numerical simulation of steady, non-evaporating hollow-cone sprays interacting with concentric annular air jets is performed using the discrete stochastic particle method in KIVA. The spray characteristics such as SMD, mean droplet velocity, liquid volume flux, air/liquid mass ratio, and droplet number density arc obtained and compared with the measurements involving different air flow rates in large and small annuli. Overall satisfactory agreement is achieved between calculation and experiment except for the deviation in the downstream SMD arising from uncertainty in the size distribution function at injection, and inaccuracy in the averaged spray parameters due to the small volumes of axisymmetric 2-D sector meshes close to the axis.

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석유팬히터 기화기내 유동장 해석 (Numerical Analysis of Kerosene Burner)

  • 홍용주;심성훈;김인규;김영수
    • 연구논문집
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    • 통권27호
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    • pp.109-118
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    • 1997
  • Kerosene Burner has widely used in domestic heating appliance. Higher combustion efficiency is required to save fuel and clean exhaust gas. The combustion characteristics in kerosene burner highly depends on the performance of evaporating liquid kerosene. And performance of evaporating effect on generation of tar. In this study, flow and heat transfer of kerosene burner is simulated by FLUENT/UNS using unstructured mesh system and discrete phase model to analyze performance of evaporating kerosene liquid. The simulated results show very complicated flow pattern and back flow at the exit of burner.

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Spray Structures and Vaporizing Characteristics of a GDI Fuel Spray

  • Park, Dong-Seok;Park, Gyung-Min;Kim, Duck-Jool
    • Journal of Mechanical Science and Technology
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    • 제16권7호
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    • pp.999-1008
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    • 2002
  • The spray structures and distribution characteristics of liquid and vapor phases in non-evaporating and evaporating Gasoline Direct Injection (GDI) fuel sprays were investigated using Laser Induced Exciplex Fluorescence (LIEF) technique. Dopants were 2% fluorobenzene and 9% DEMA (diethyl-methyl-amine) in 89% solution of hexane by volume. In order to study internal structure of the spray, droplet size and velocity under non-evaporating condition were measured by Phase Doppler Anemometry (PDA). Liquid and vapor phases were visualized at different moments after the start of injection. Experimental results showed that the spray could be divided into two regions by the fluorescence intensity of liquid phase: cone and mixing regions. Moreover, vortex flow of vapor phase was found in the mixing region. About 5㎛ diameter droplets were mostly distributed in the vortex flow region. Higher concentration of vapor phase due to vaporization of these droplets was distributed in this region. Particularly, higher concentration of vapor phase and lower one were balanced within the measurement area at 2ms after the start of injection.

고압 상태에서의 연료 분무의 증발 및 연소 특성 해석 (Numerical Studies on Vaporization Characterization and Combustion Processes in High-Pressure Fuel Sprays)

  • 문윤완;김용모;김세원;김주연;윤인용
    • 한국분무공학회지
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    • 제3권3호
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    • pp.49-59
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    • 1998
  • The vaporization characteristics and spray combustion processes in the high-pressure environment are numerically investigated. This study employ the high-pressure vaporization model together with the state-of-art spray submodels. The present high-pressure vaporization model can account for transient liquid heating, circulation effect inside the droplet forced convection, Stefan flow effect, real gas effect and ambient gas solubility in the liquid droplets. Computations are carried out for the evaporating sprays, the evaporating and burning sprays, and the spray combustion processes of the turbocharged diesel engine. Numerical results indicate that the high-pressure effects are quite crucial for simulating the spray combustion processes including vaporization, spray dynamics, combustion, and pollutant formation.

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마이크로핀 관의 기하학적 형상면화에 대한 열전달 특성(II) -증발 열전달- (Heat transfer with geometric shape of micro-fin tubes (II) -Evaporating heat transfer-)

  • 곽경민;장재식;배철호;정모
    • 설비공학논문집
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    • 제11권6호
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    • pp.789-798
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    • 1999
  • The evaporating heat transfer experiments with refrigerant HCFC 22 are performed for performance evaluation using 4 and 6 kinds of microfin tubes with outer diameter of 9.52mm and 7.0mm, respectively. Used microfin tubes have different shape and number of fins with each other, The experimental results are represented with effects of quality, mass flux and EPR. The evaporating heat transfer characteristics are represented by the existence of not only heat transfer area and turbulence promotion effect but also additional other enhancement mechanism, which are the overflow of the refrigerant over the microfin and microfin arrangement. Microfin tubes having a shape which can give much overflow over the microfin show large evaporating heat transfer coefficients. The effect of refrigerant overflow is much severe in evaporation than condensation. The effect of microfin arrangement is related to overflow effect of the refrigerant over the microfin.

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주위조건 변화에 대한 증발 디젤분무 거동특성 연구 (Study on the Behavior Characteristics of the Evaporative Diesel Spray under Change in Ambient Conditions)

  • 염정국
    • 대한기계학회논문집B
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    • 제33권6호
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    • pp.454-460
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    • 2009
  • To analyze the mixture formation process of evaporating diesel spray is important for emissions reduction in actual engines. Then the effects of change in density of ambient gas on spray structure in high temperature and pressure field have been investigated in this study. The ambient gas density was changed from ${\rho}_a=5.0kg/m^3$ to ${\rho}_a=12.3kg/m^3$ with CVC(Constant Volume Chamber). Also, simulation study by modified KIVA-II code was conducted and compared with experimental results. The ambient temperature and injection pressure are kept as 700K and 72MPa, respectively. The images of liquid and vapor phase in the evaporating free spray were simultaneously taken by exciplex fluorescence method. As experimental results, with increasing ambient gas density, the tip penetration of the evaporating free spray decreases due to the increase in the drag force from ambient gas. The spatial structure of a diesel spray can be verified as 2-regions consisted of liquid with momentum decrease and vapor with large-scale vortex. The calculated results obtained by modified KIVA-II code show good agreements with experimental results.