• 제목/요약/키워드: Droplet velocity

검색결과 345건 처리시간 0.028초

소형 액체로켓엔진 인젝터 분무의 연료분사압력 변이에 따른 액적의 공간분포 특성 (Spatial Distribution Characteristics of Small LRE-injector's Spray-droplet According to the Variation of Fuel-injection Pressure)

  • 정훈;김정수
    • 한국추진공학회지
    • /
    • 제12권5호
    • /
    • pp.1-8
    • /
    • 2008
  • 소형 액체로켓엔진 인젝터 분무의 공간분포 특성 규명을 위해 이중모드 위상도플러속도계(DPDA)를 이용한다. 분사압력 및 분무확산방향 이동거리를 변화시켜 분무액적의 크기, 속도 등을 측정하고, 산술평균직경(AMD), Sauter 평균직경(SMD), 수밀도, 스팬(span of drop size distribution), 그리고 체적 유속(volume flux) 등의 분무 매개변수를 도출하여 인젝터 분무의 분열특성을 고찰한다. 분사압력이 증가함에 따라 분무액적의 수밀도, 스팬, 그리고 체적 유속은 증가하지만, AMD는 감소하였다.

배관 재질 손상에 미치는 액적충돌침식의 영향에 대한 연구 (A Study for the Effect of Liquid Droplet Impingement Erosion on the Loss of Pipe Flow Materials)

  • 김경훈;조연수;김형준
    • 한국분무공학회지
    • /
    • 제18권1호
    • /
    • pp.9-15
    • /
    • 2013
  • Wall thinning of pipeline in power plants occurs mainly by flow acceleration corrosion (FAC), cavitation erosion (C/E), liquid droplet impingement erosion (LDIE). Wall thinning by FAC and C/E has been well investigated; however, LDIE in plant industries has rarely been studied due to the experimental difficulty of setting up a long injection of highly-pressurized air. In this study, we designed a long-term experimental system for LDIE and investigate the behavior of LDIE for three kinds of materials (A106B, SS400, A6061). The main control parameter was the air-water ratio (${\alpha}$), which was defined as the volumetric ratio of water to air (0.79, 1.00, 1.72). In order to clearly understand LDIE, the spraying velocity (${\nu}$) of liquid droplets was controled larger then 160 m/s and the experiments were performed for 15 days. Therefore, this research focuses relation between erosion rate and air-water ratio on the various pipe-flow materials. NPP(nuclear power plant)'s LDIE prediction theory and management technique were drawn from the obtained data.

Computations of Droplet Impingement on Airfoils in Two-Phase Flow

  • Kim, Sang-Dug;Song, Dong-Joo
    • Journal of Mechanical Science and Technology
    • /
    • 제19권12호
    • /
    • pp.2312-2320
    • /
    • 2005
  • The aerodynamic effects of leading-edge accretion can raise important safety concerns since the formulation of ice causes severe degradation in aerodynamic performance as compared with the clean airfoil. The objective of this study is to develop a numerical simulation strategy for predicting the particle trajectory around an MS-0317 airfoil in the test section of the NASA Glenn Icing Research Tunnel and to investigate the impingement characteristics of droplets on the airfoil surface. In particular, predictions of the mean velocity and turbulence diffusion using turbulent flow solver and Continuous Random Walk method were desired throughout this flow domain in order to investigate droplet dispersion. The collection efficiency distributions over the airfoil surface in simulations with different numbers of droplets, various integration time-steps and particle sizes were compared with experimental data. The large droplet impingement data indicated the trends in impingement characteristics with respect to particle size ; the maximum collection efficiency located at the upper surface near the leading edge, and the maximum value and total collection efficiency were increased as the particle size was increased. The extent of the area impinged on by particles also increased with the increment of the particle size, which is similar as compared with experimental data.

Behavior of contaminated liquid CO2 droplets in the deep sea

  • Nguyen, Thao;Hwang, Jin Hwan
    • 한국수자원학회:학술대회논문집
    • /
    • 한국수자원학회 2015년도 학술발표회
    • /
    • pp.257-257
    • /
    • 2015
  • Carbon Capture and Storage with ocean sequestration is being considered as one of the most effective option for reducing the $CO_2$ net flux from atmosphere nowadays. But it is still possible for $CO_2$ substance to leaks out from transport pipeline or from the under seabed storage sites and causing damage to ambient environment. The behavior of liquid $CO_2$ under droplet shape would be strongly affected by the presence of other contaminants such as $SO_2$ comes from processing processes. This presentation shows the behavior in the sea water of pure liquid $CO_2$ droplets as well as droplets that consist of $SO_2$ substances. The study uses computational fluid dynamic models in comparison with experimental data from other previous researchers. Droplet of liquid $CO_2$ is assumed to be released at several depths in deep ocean, with other environmental conditions are set up respectively. All calculations are conducted with many different ratio of contaminant $SO_2$ to provide fundamental data of those particles rising characteristics. The effect of contaminants on the behavior of $CO_2$ droplets would be clearly shown through the results of particle deformation, terminal rising velocity happen due to buoyancy force driving from the difference in density of $CO_2$ substance and ocean water around.

  • PDF

스프링클러 분무 해석에 영향을 미치는 통계적액적군집의 영향 (Effect of the Statistical Droplet Parcel on Numerical Simulation of Sprinkler Spray)

  • 김성찬;이상우;박원주
    • 한국화재소방학회:학술대회논문집
    • /
    • 한국화재소방학회 2008년도 추계학술논문발표회 논문집
    • /
    • pp.363-370
    • /
    • 2008
  • The present study has been performed to investigate the effect of statistical number of droplets on the simulation of the sprinkler spray using fire field model. In order to simulate the sprinkler spray characteristics, the present study uses NIST Fire Dynamics Simulator version 5.2. A group of Lagrangian particle with similar droplet characteristics, such as diameter, velocity, temperature and so on, is represented by parcel concept to decrease the total number of droplets tracked in the simulation. The present study introduces a new parameter to represent the ratio between real number of droplets and computational parcels. The dependency of the number of parcels on the fire suppression characteristics and spray patterns is quantitatively examined for different ratio between the real number of droplets and computational parcels.

  • PDF

고온 강판의 분무냉각에 있어서 MHF 점에 관한 연구 (Study on Minimum Heat Flux Point in Spray Cooling of Hot Plate)

  • 김영찬
    • 대한기계학회:학술대회논문집
    • /
    • 대한기계학회 2001년도 춘계학술대회논문집D
    • /
    • pp.175-180
    • /
    • 2001
  • In this study, the minimum heat flux conditions are experimentally investigated for the spray cooling of hot plate. The hot plates are cooled down from the initial temperature of about $900^{\circ}C$, and the local heat flux and surface temperatures are calculated from the measured temperature-time history. The results show that the minimum heat flux point temperatures increase linearly resulting from the propagation of wetting front with the increase of the distance from the stagnation point of spray flow. However, in the wall region, the minimum heat flux point temperature becomes independent of the distance. Also, the experimental results show that the velocity of wetting front increases with the increase of the droplet flow rate.

  • PDF

슬링거 연소기의 회전형 분사장치의 분무특성 연구 (Spray Characteristics of the Rotary Atomizer for the Slinger Combustor)

  • 최현경;이동훈;유경원;최성만
    • 한국분무공학회지
    • /
    • 제13권3호
    • /
    • pp.149-155
    • /
    • 2008
  • An experimental study was performed to understand spray characteristics of the rotary atomizer for the slinger combustor. In this fuel injection system, fuel is injected and atomized in the combustor by centrifugal forces to engine shaft. The experimental apparatus consists of a high speed rotational spindle, rotary atomizer, pressure tank and acrylic case. The droplet size and velocity were measured by PDPA (phase Doppler particle analyzer), and spray was visualized by using high speed camera and Nd:Yag laser-based flash photography. From the test results, the droplet size (SMD) is largely affected by rotational speed, mass flow rate and the number of orifice. As the experimental results, we could understand the spray characteristics of the rotary atomizer for the slinger combustor and obtain the optimum shape of the rotary atomizer which is suitable for the small gas turbine engine.

  • PDF

난류선회 등온 및 분무연소 유동에 대한 수치해석 (Numerical Study of Turbulent Swirling Isothermal and Spray-Combusting Flows)

  • 김성구;안국영;김용모;이창식
    • 한국자동차공학회논문집
    • /
    • 제4권5호
    • /
    • pp.130-141
    • /
    • 1996
  • Numerical study of a confined, swirling, isothermal and spray-combusting flows has been presented. The pressure-velocity coupling in the Eulerian gas-phase equation is handled by the improved PISO algorithm. The droplet dispersion by turbulence is introduced by a Stochastic Separated Flow(SSF) model. The k-$\varepsilon$ turbulence model and the eddy dissipation model are employed to account for turbulence-combustion interaction. The detailed comparison with experimental data has been made for the isothermal jet swirling flows and the nearly monodisperse spray-combusting flow in the swirl combustor.

  • PDF

Molecular Dynamics Study on the Binary Collision of Nanometer-Sized Droplets of Liquid Argon

  • Chun, In-Beom;Ha, Man-Yeong;Jang, Joon-Kyung;Yoon, Hyun-Sik
    • Bulletin of the Korean Chemical Society
    • /
    • 제32권6호
    • /
    • pp.2027-2031
    • /
    • 2011
  • Molecular dynamics simulation is used to study the binary collisions of nanometer-sized droplets of argon in the presence of a surrounding gas. By systematically varying the droplet size, the impact parameter and the velocity of collision, the outcome of such collisions were examined and they can be classified into coalescence, separation and shattering. If one of the colliding droplets is half or less than the other in diameter, a shattering is not possible to occur. The threshold of impact parameter for a given separation was studied by adjusting the Weber number. Overall nanoscale droplets were more likely to coalesce than the macroscopic sized ones due to their high surface-to-volume ratio.

Spray and Atomization Technologies in Pesticides Application: A Review

  • No, Soo-Young
    • 한국분무공학회지
    • /
    • 제6권4호
    • /
    • pp.1-13
    • /
    • 2001
  • In the pesticides sprays, spray and atomization technologies to increase the deposition and reduce the drift are briefly reviewed. Further research is needed to deduce a measure of drift risk in sprays with different structures, velocity profiles. For flat fan nozzles, the data of breakup length and thickness of liquid sheet are essential to understand the atomization processes and develop the transport model to target. In the air-assisted spray technology to reduce drift, further works on the effect of application height on drift and air assistance on droplet size should be followed. In addition, methods for quantifying included air in the air inclusion techniques are required. A few researches on the droplet size of fallout can be found in the literature. A combined technology with electrostatic method into one of method for the reduction of drift may be an effective strategy for increasing deposition and reducing drift.

  • PDF