• Title/Summary/Keyword: vaporization

Search Result 453, Processing Time 0.029 seconds

Vaporization Characteristics of Dodecane Fuel Droplet in Supercritical Condition (도데케인 연료액적의 초임계 상태 기화 특성)

  • Ko, J.B.;Lee, K.H.;Koo, J.Y.;Jeon, C.S.;Moon, H.J.
    • Journal of ILASS-Korea
    • /
    • v.9 no.3
    • /
    • pp.8-14
    • /
    • 2004
  • Characteristics of droplet vaporization at high ambient pressures and temperatures which are supercritical conditions is studied numerically by formulating one dimensional vaporization model in liquid dodecane and air. Modified Soave-Redlich-Kwong state equation is used to condider real gas effect. Non-ideal behavior of properties at near critical and supercritical conditions is considered in the high pressure condition. Characteristic spatial distribution of properties with various conditions of pressure and temperature is evaluated in order to understand vaporizing evolution.

  • PDF

Numerical Analysis of Spray Behavior and Vaporization Characteristic of GDI Engine Injector Under Ambient Conditions (분위기 조건에 따른 GDI 엔진용 인젝터의 분무거동 및 증발특성에 대한 수치적 해석)

  • Shim, Young-Sam;Hwang, Soon-Chul;Kim, Duck-Jool
    • Transactions of the Korean Society of Mechanical Engineers B
    • /
    • v.28 no.5
    • /
    • pp.545-552
    • /
    • 2004
  • The purpose of this study is to improve the prediction ability of the atomization and vaporization processes of GDI spray. Several models have been introduced and compared. The atomization process was modeled using hybrid breakup model that is composed of Linearized Instability Sheet Atomization (LISA) model and Aerodynamically Progressed TAB (APTAB) model. The vaporization process was modeled using Spalding model and Abramzon & Sirignano model. Exciplex fluorescence method was used for comparing calculated with experimental results. The experiment and computation were performed at the ambient pressure of 0.1 MPa, 0.5 MPa and 1.0 MPa and the ambient temperature of 293k and 473k. Comparison of calculated and experimental spray characteristics was carried out and the calculated results of GDI spray showed good agreement with experimental results.

Analysis of Nanosecond Explosive Vaporization Process by Photothermal/Photoacoustic Methods (광열/광음 기법에 의한 나노초 폭발적 기화 과정 분석)

  • Park, Hee-K.;Grigoropoulos, Costas P.;Choi, Sun R.;Kim, Dong-Sik
    • Transactions of the Korean Society of Mechanical Engineers B
    • /
    • v.27 no.6
    • /
    • pp.804-812
    • /
    • 2003
  • This paper introduces optical methods for in-situ measurement of surface temperature and pressure transient in thermal processes having nanosecond time scales. In the temperature measurement, a p -Si thin film whose refractive index is calibrated as a function of temperature is embedded beneath the sample surface and the photothermal reflectance is monitored for estimating the surface temperature. The pressure transients are measured using the photoacoustic optical deflection method. The experimental technique is used to analyze the nanosecond laser induced vaporization process that is central to numerous engineering and bio-medical applications. Based on the experimental results, discussions are made on the experimental technique and the physical mechanisms of laser-driven explosive vaporization phenomena.

Molecular Dynamics Simulation of Droplet Vaporization (분자 동력학을 이용한 액적 기화 시뮬레이션)

  • Nam, Gun-Woo;Yoon, Woong-Sup
    • Proceedings of the KSME Conference
    • /
    • 2003.11a
    • /
    • pp.121-126
    • /
    • 2003
  • A study of argon droplet vaporization is conducted using molecular dynamics, instead of using traditional methods such as the Navier-Stokes equation. Molecular dynamics uses Lagrangian frame to describe molecular behavior in a system and uses only momentum and position data of all molecules in the system. So every property is not a hypothetical input but a statistical result calculated from the momentum and position data. This work performed a simulation of the complete vaporization of a three dimensional submicron argon droplet within quiescent environment. Lennard-Jones 12-6 potential function is used as a intermolecular potential function. The molecular configuration is examined while an initially non-spherical droplet is changed into the spherical shape and droplet evaporates. And the droplet radius versus time is calculated with temperature and pressure profile.

  • PDF

Sensitivity of EOS in Analyzing the High-Pressure Vaporization Characteristics (고압 상태의 증발 특성 해석결과에 미치는 상태방정식의 영향)

  • You, Y.W.;Kim, Y.M.
    • Journal of ILASS-Korea
    • /
    • v.2 no.3
    • /
    • pp.32-43
    • /
    • 1997
  • A comparison of predicted molar volume, vapor - liquid equilibrium, enthalpy of vaporization, droplet size history. and vaporization rates with several forms of equation of state has been made. The equation of state (EOS) investigated in this study includes the EOS given by Redlich - Kwong, the Soave - Redlich - Kwong, and the Peng - Robinson. Numerical results indicate that the Peng - Robinson EOS yields more accurate predictions of vapor - liquid equilibrium under a broader range of temperature and pressure conditions, especially at high pressures and near the critical point.

  • PDF

Responses of Droplet Evaporation to High-Pressure Oscillations (강한 압력 교란에 구속된 고압 액적의 연소 응답)

  • Kim, Sung-Yup;Yoon, Woong-Sup
    • Proceedings of the KSME Conference
    • /
    • 2004.04a
    • /
    • pp.1286-1291
    • /
    • 2004
  • In order for studying pressure-coupled dynamic responses of droplet vaporization, open-loop experiment of an isolated droplet vaporization exposed to pressure perturbations in stagnant gaseous environment is numerically conducted. Governing equations are solved for flow parameters at gas and liquid phases separately and thermodynamic parameters at the interfacial boundary are matched for problem closure. For high-pressure effects, vapor-liquid interfacial thermodynamics is rigorously treated. A series of parametric calculations in terms of mean pressure level and wave frequencies are carried out employing a n-pentane droplet in stagnant gaseous nitrogen. Results show that wave instability in view of pressure-coupled vaporization response seems more susceptible at higher pressures and higher wave frequencies. Mass evaporation rate responding to pressure waves is amplified with increase in pressure due to substantial reduction in latent heat of vaporization. Augmentation of perturbation frequency also enhances amplification due to the reduction of phase differences between pressure perturbation and surface temperature fluctuation.

  • PDF

Vaporization Characteristics of Liquid Oxygen at High-Pressure Environment (고압 상태에서의 액체 산소의 증발 특성 해석)

  • 유용욱;김용모;손정락
    • Journal of the Korean Society of Propulsion Engineers
    • /
    • v.2 no.3
    • /
    • pp.90-98
    • /
    • 1998
  • The vaporization process of liquid oxygen(LOX) at high pressure environment is numerically investigated. The present vaporization model can account for the high-pressure effects such as ambient gas solubility, real gas behavior and variable properties. The predicted phase-equilibrium compositions for $N_2$/$H_2$ and $O_2$/He system are well agreed with experimental data. The LOX vaporization characteristics is parametrically studied for wide range of the operating conditions encountered in the high-pressure combustion process of liquid rocket engine.

  • PDF

Numerical Studies on the Combustion Characteristics and Pollutant Formation for the DME Fueled Diesel Engine (DME 연료 디젤엔진의 연소 및 공해물질 배출 특성 해석)

  • Yu, Yong-Wook;Lee, Jeong-Won;Kim, Yong-Mo
    • Journal of ILASS-Korea
    • /
    • v.13 no.1
    • /
    • pp.28-33
    • /
    • 2008
  • The present study is mainly motivated to investigate the vaporization, auto-ignition and combustion processes in high-pressure diesel engines. In order to realistically simulate the dimethyl ether (DME) fueled diesel engine, the high pressure vaporization model is utilized and the interaction between turbulence and chemistry is treated by employing the Representative Interactive Flamelet (RIF) model. The detailed chemisty consisted of 336 elementary reaction steps and 78 species is used for DME/air reaction. Numerical results indicate that the RIF model with high pressure vaporization model successfully predicts the essential feature of the combustion processes and pollutants formations in the DME fueled diesel engines.

  • PDF

Determination of Oxygen Diffusion Coefficient from Vaporization Rate of MgO.$nAl_2O_3$ Spinel (MgO.$nAl_2O_3$ 스피넬에 대한 증발속도의 측정으로부터 산소의 확산계수의 결정)

  • 이홍림;배철훈
    • Journal of the Korean Ceramic Society
    • /
    • v.20 no.2
    • /
    • pp.129-134
    • /
    • 1983
  • MgO.$Al_2O_3$ polycrstalline spinel powder was subjected to vaporization over the temperature range of 1150-130$0^{\circ}C$ under H2 atmosphere. Diffusion coefficient of oxygen ion through the spinel were calculated using the measure vaporization rates as follows : D=28.4 exp(-901500/RT) Reference data of the vaporization rates of MgO.$8Al_2O_3$ single crystal spinel were applied to the vaporiza-tion model proposed in this study and were calculated to give the oxygen ion diffusion coefficients over the tempera-ture 1700-195$0^{\circ}C$. The obtained diffusion coefficients are as follows: $D=3.20{\times}106$ exp(-155600/RT)

  • PDF

A Study of Vaporization Characteristics in the Methanol Spark Ignition Engine (메탄올 스파크 점화기관의 기화특성에 관한 연구)

  • 한성빈;문성수;이성열
    • Transactions of the Korean Society of Mechanical Engineers
    • /
    • v.18 no.1
    • /
    • pp.77-84
    • /
    • 1994
  • The oil crises in 1973 and 1978 stimulated the alternative fuel research activities in many countries around the world. Among the alternative fuels, methanol is one of the highest potential fuels for transportation. Methanol has been considered for use as automotive fuel, but it has a defect of the great latent vaporization heat. Therefore, authors have made the fuel vaporizing device in order to eliminate the fuel film flow heating the mixture. This paper presents a study on the characteristics of vaporization, engine performance, and emission which result from using the fuel vaporizing device.