• 제목/요약/키워드: Liquid Transient

검색결과 394건 처리시간 0.022초

플래시 상평형 방법에 의한 고압 액적 기화 모델 (Modeling of High Pressure Droplet Vaporization with Flash Phase Equilibrium Calculation)

  • 이강원;윤웅섭
    • 한국추진공학회:학술대회논문집
    • /
    • 한국추진공학회 2002년도 제18회 학술발표대회 논문초록집
    • /
    • pp.65-69
    • /
    • 2002
  • Unsteady vaporization of a droplet quiescent in a high pressure environment are studied with emphasis placed oil the modeling of equilibrium at vapor-liquid interface. Complete set of conservation equations for liquid and gas phases is numerically time integrated. Vapor-liquid interfacial thermodynamics are solved by f]ash equilibrium calculation method. The model was proper]y validated with experiment and the improvement in the solution accuracy was made. Vaporization of n-pentane fuel droplet in nitrogen background gas is examined. Effects of ambient gas solubility, property variation, transient diffusion, and multicomponent transport on the droplet vaporization are investigated systematically. High-pressure effects on the droplet vaporization is examined and discussed.

  • PDF

대추력 액체로켓엔진 예비설계 프로그램 : 비정상작동.동특성 예측 기술 개요 및 현황 (Preliminary Design Program for a High Thrust Liquid Rocket-Engine : Dynamic Characteristic Prediction Program Overview and Technical Achievements)

  • 고태호;김상민;김형민;윤웅섭
    • 한국추진공학회:학술대회논문집
    • /
    • 한국추진공학회 2009년도 춘계학술대회 논문집
    • /
    • pp.417-418
    • /
    • 2009
  • Aiming at time-dependent performance prediction of Liquid Rocket Engine(LRE) system, Program for Dynamic Characteristic Prediction of LRE is overviewed, and a modeling and dynamic analysis of rocket engine system with reference to developed transient simulator for LRE is outlined.

  • PDF

대추력 액체로켓엔진 예비설계 프로그램 : 정상성능 설계를 위한 구성품 모델링 (Preliminary Design Program for a High Thrust Liquid Rocket-Engine : Components Design for Static Performance Design)

  • 고태호;김상민;김형민;윤웅섭
    • 한국추진공학회:학술대회논문집
    • /
    • 한국추진공학회 2009년도 춘계학술대회 논문집
    • /
    • pp.414-416
    • /
    • 2009
  • In order to build a transient simulation program for a high thrust liquid rocket engine(LRE), a static performance simulation program for components were made. The components were the thrust chamber (combustion chamber and supersonic nozzle), centrifugal pump (impeller and volute casing), impulse turbine, and flow control devices (control valve and orifice). Simplified mathematical models based on classical thermodynamic and inviscid theories were used to remove complexity and enhance the utility of the program. We examined the results of each program qualitatively for validate each component modeling.

  • PDF

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
    • /
    • 제3권3호
    • /
    • pp.49-59
    • /
    • 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.

  • PDF

DME 및 n-Heptane 연료의 디젤엔진 조건에서 분무연소특성 해석 (Numerical Study on the Characteristics of Spray Combustion Processes in the DME and n-heptane Fueled Diesel-like Engine Conditions)

  • 유용욱;석준호;이상길;김용모
    • 한국분무공학회지
    • /
    • 제13권2호
    • /
    • pp.91-98
    • /
    • 2008
  • In the present study, in order to understand the overall spray combustion characteristics of DME fuel as well as to identify the distinctive differences of DME combustion processes against the conventional hydrocarbon liquid fuels, the sequence of the comparative analysis have been systematically made for DME and n-heptane liquid fuels. To realistically represent the physical processes involved in the spray combustion, this studyemploys the hybrid breakup model, the stochastic droplet tracking model, collision model, high-pressure evaporation model, and transient flamelet model with detailed chemistry. Based on numerical results, the detailed discussions are made in terms of the autoignition, spray combustion processes, flame structure, and turbulence-chemistry interaction in the n-heptane and DME fueled spray combustion processes.

  • PDF

A negative reactivity feedback driven by induced buoyancy after a temperature transient in lead-cooled fast reactors

  • Arias, Francisco J.
    • Nuclear Engineering and Technology
    • /
    • 제50권1호
    • /
    • pp.80-87
    • /
    • 2018
  • Consideration is given to the possibility to use changes in buoyancy as a negative reactivity feedback mechanism during temperature transients in heavy liquid metal fast reactors. It is shown that by the proper use of heavy pellets in the fuel elements, fuel rods could be endowed with a passive self-ejection mechanism and then with a negative feedback. A first estimate of the feasibility of the mechanism is calculated by using a simplified geometry and model. If in addition, a neutron poison pellet is introduced at the bottom of the fuel, then when the fuel element is displaced upward by buoyancy force, the reactivity will be reduced not only by disassembly of the core but also by introducing the neutron poison from the bottom. The use of induced buoyancy opens up the possibility of introducing greater amounts of actinides into the core, as well as providing a palliative solution to the problem of positive coolant temperature reactivity coefficients that could be featured by the heavy liquid metal fast reactors.

액적 열전달 향상에 미치는 Dissolved 가스의 영향에 관한 연구 (Effect of Dissolved Gases on Liquid Droplet Heat Transfer Enhancement)

  • 이정호
    • 대한기계학회:학술대회논문집
    • /
    • 대한기계학회 2003년도 춘계학술대회
    • /
    • pp.1491-1498
    • /
    • 2003
  • Droplet evaporation can be used to transfer large amounts of energy since heat is transferred across a thin liquid film. Spreading the drop over a larger area can enhance this heat transfer. One method of accomplishing this is to dissolve gas into the liquid. When the drop strikes the surface, a gas bubble nucleates and can grow and merge within the liquid, resulting in an increase in the droplet diameter. In this study, time and space resolved heat transfer characteristics for a single droplet striking a heated surface were experimentally investigated. The local wall heat flux and temperature measurements were provided by a novel experimental technique in which 96 individually controlled heaters were used to map the heat transfer coefficient contour on the surface. A high-speed digital video camera was used to simultaneously record images of the drop from below. The measurements to date indicate that significantly smaller droplet evaporation times can be achieved. The splat diameter was observed to increase with time just after the initial transient dies out due to the growth of the bubble, in contrast to a monotonically decreasing splat diameter for the case of no bubbles. Bursting of the bubble corresponded to a sudden decrease in droplet heat transfer.

  • PDF

An electric conductive-probe technique for measuring the liquid fuel layer in the intake manifold

  • Kajitani, S.;Sawa, N.;Rhee, K.T.;Hayashi, S.
    • 제어로봇시스템학회:학술대회논문집
    • /
    • 제어로봇시스템학회 1990년도 한국자동제어학술회의논문집(국제학술편); KOEX, Seoul; 26-27 Oct. 1990
    • /
    • pp.1184-1189
    • /
    • 1990
  • In order to investigate liquid fuel filming over the intake manifold wall, an electrode-type probe has been developed by lines of authors and this probe was employed in a single cylinder two and four-stroke cycle engine and in a four cylinder four-stroke engine operated by neat methanol fuel. The performance of the probe was dependent upon several parameters including the liquid fuel layer thickness, temperature, additive in the fuel, and electric power source (i.e., AC and voltage level) and was independent of other variables such as direction of liquid flow with respect to the probe arrangement. Several new findings from this study may be in order. The flow velocity of the fuel layer in the intake manifold of engine was about (if the air velocity in the steady state operation, the layer thickness of liquid fuel varied in both the circumferential and longitydinal directions. In the transient operation of the engine, the temporal variation of fuel thickness was determined, which clearly suggests that there was difference between fuel/air ratio in the intake manifold and that in the cylinder. The variation was greatly affected by the engine speed, fuel/air ratio and throttle opening. And the variation was also very significant from cylinder to cylinder and it was particularly strong different engine speeds and throttle opening.

  • PDF

과냉 액체질소 내에서 순간적 열확산 실험 (Thermal diffusion experiment of impulsive heat in subcooled liquid nitrogen)

  • 최진혁;하찬준;변정주;장호명;김호민;고태국
    • 한국초전도ㆍ저온공학회논문지
    • /
    • 제8권1호
    • /
    • pp.65-70
    • /
    • 2006
  • Transient heat transfer caused by an impulsive heating in subcooled liquid nitrogen is investigated experimentally. This study is part of out ongoing efforts directed to a stable cryogenic cooling system lot superconducting fault current limiters (SFCL). A thin heater attached by epoxy on one surface of a GFRP plate is immersed in liquid-nitrogen bath at temperatures between 77 K and 55 K. A strong heat flux up to $150W/cm^2$ is generated lot 100 ms, and the temperature of the heater sulfate is measured as a function of time. The behavior of bubbles on the heating surface can be explained by comparing the measured temperature history for vertical and two horizontal (up and down) orientations. It is concluded that the subcooling of liquid nitrogen below 70 K is very effective in suppressing bubbles, resulting in better thermal protection and faster recovery from an impulsive heat.

소듐분위기에서 물 누출로 인한 Ferrite Steel에서의 반응현상 (Reaction Phenomena of the Ferrite Steel by Water Leakage into Liquid Sodium)

  • 정경채;김병호;권상운;김광락;황성태
    • 공업화학
    • /
    • 제9권2호
    • /
    • pp.268-272
    • /
    • 1998
  • 액체금속로 냉각재인 액체 소듐에서 시편의 누출특성을 소듐-물 반응 실험에 의해 조사하였다. 소듐-물 반응 현상의 확인은 물 누출 실험 전후에 Fe, Cr 및 Ni 등과 같은 시편의 조성 변화로 확인하였다. $100kg/cm^2$의 누출 압력으로 4시간 동안 시편의 누출 경로를 통해 물을 누출시킨 결과, 누출경로에서 소듐-물 반응생성물들이 침적되어 있는 것을 확인하였으나, 부식에 의해 누출경로가 완전 파열되어 다량의 수증기가 액체 소듐속으로 빠져나가는 re-openning 현상은 관찰되지 않았다. 시편의 누출경로가 막히는 self-plugging 현상은 소듐-물 반응에 의한 반응생성물과 시편의 부식에 의한 부식 생성물이 주 원인으로 추정되고, re-openning 현상은 시편의 누출경로에서 열적인 transient로 추정되었다.

  • PDF