• Title/Summary/Keyword: Two-flow nozzle

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Collection Efficiency Enhancement of Spray Tower Scrubber by Introducing Electrospray with Two-flow Nozzle (분무탑식 스크러버에서 이류체 정전분무에 의한 집진효율의 향상)

  • Hwang, You-Seong;Kim, Jong-Ho;Kim, Jong-Hyeon
    • Journal of Korean Society for Atmospheric Environment
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    • v.26 no.3
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    • pp.339-345
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    • 2010
  • There have been a number of efforts to satisfy national emission regulations and reduce the amount of emitted air pollutants. There are several air pollution control devices, however, only wet scrubber is efficiently used to remove particulate matters and gaseous pollutants, even if it has minimum collection efficiency in the particle size range of $0.1{\sim}1{\mu}m$. This study aimed to improve the collection efficiency of a spray tower type scrubber by introducing an electrospray system with two-flow nozzle. We found that the collection efficiency of a spray tower type scrubber was similar to that of a conventional wet scrubber. However, installation of an electrospray system in the scrubber resulted in drastic further improvement of collection efficiency comparing to that of a conventional scrubber, which is 26%, 35.2%, and 45.1% at the liquid to gas ratio of 0.26 $L/m^3$ and 19.9%, 35.1%, and 42.5% at 0.34 $L/m^3$ for the applied voltage of -30 kV, -35 kV, and -40 kV, respectively. Therefore, we found that the introduction of an electrospray system is very effective to improve the collection efficiency of a spray tower type scrubber.

Comparative Studies of Heat Transfer Coefficients for Rocket Nozzle (로켓 노즐의 열전달계수 비교 연구)

  • Hahm, Hee-Cheol;Kang, Yoon-Goo
    • Journal of the Korean Society of Propulsion Engineers
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    • v.16 no.2
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    • pp.42-50
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    • 2012
  • The goal of heat transfer studies is the accurate prediction of temperature and heat flux distribution on material boundaries. To this purpose, general-purpose computational fluid dynamics(CFD) code is used : FLUENT. Mass fluxes and pressure ratio are calculated for two types of nozzle. The comparative studies reveal that the computational results are in agreement with the experimental data. Also, heat transfer coefficients from FLUENT for one type of nozzle are very similar and agree well with the experimental data in the diverging part of the nozzle, but the calculated results are large in the converging part. The heat transfer coefficients from Bartz equation are over-predicted. We can consider various reasons for these differences, i.e., laminarization by the highly accelerated flow in the nozzle, turbulent flow model and grid generation.

An Experimental Study on the Flow Characteristics with the Impinging Angles of Defrost Nozzle Jet Inside a Vehicle Passenger Compartment (차실내 Defrost 노즐 분류의 충돌각 변화에 따른 유동특성에 관한 실험적 연구)

  • Kim, Duck-Jin;Kim, Hyun-Joo;Rho, Byung-Joon;Lee, Jee-Keun
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.31 no.12
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    • pp.1024-1032
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    • 2007
  • The flow characteristics with the impinging angles of defrost nozzle jet inside a commercial vehicle passenger compartment were investigated experimentally by using the two-dimensional duct-nozzle model. The shape of the nozzle contraction was designed according to the curved line of cubic equation to the vertical plan of the flow direction. The impinging angles, defined as the angle between nozzle axis and a vertical line to the windshield, were varied from the $0^{\circ}\;to\;80^{\circ}$. The mean velocity distributions, the half-widths, and the momentum distributions with the cases of both the free jet and the impinging jet onto the dummy windshield were measured. The impinging jet flows similarly with wall jet from $X/b_o=20$, and the impinging angle has an effect on the half-width of the impinging jet. The momentum distributions onto the windshield increased with the increase of impinging angle, and then their inflection point was observed around the impinging angle of $60^{\circ}$.

Experimental Study on Spray Performance of Nozzles for Autonomous Fire Fighting Monitor (자율형 소화모니터 노즐의 분사 성능에 대한 실험 연구)

  • Rhyu, SeongSun;Kim, HyoungTae;Seo, JeongHwa
    • Journal of the Society of Naval Architects of Korea
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    • v.59 no.2
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    • pp.80-88
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    • 2022
  • A systematic experimental study is carried out for the fire fighting monitor nozzle of 65A diameter to design and manufacture a new nozzle with better water spray performance than available domestic nozzles. The nozzle inlet pressure, flow rate and reach for the discharged water from the nozzle are measured by utilizing the experimental facility consisting of two pumps and piping system with a flow meter and pressure gauges. It was found that the baffle position and baffle head chamfering were the most sensitive design factors to be remarkably changed in the flow rate of the discharged water. Also, It was confirmed that the baffle position and the water exit area had the significant effect on the change in reach distance. The results obtained from this study are expected to be used effectively to design new nozzles with excellent spray performances and also to validate numerical analysis results for evaluating the water spray performance of fire fighting monitor nozzles.

An Analytical Study for Critical Mass Flowrate of Compressed Water (압축수의 임계유량에 관한 해석적 연구)

  • 김희동;김재형;한민교;박경암
    • Journal of the Korean Society of Propulsion Engineers
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    • v.7 no.1
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    • pp.57-65
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    • 2003
  • As a compressed water is rapidly expanded through a nozzle, two-phase flow of vapor and liquid is formed in the nozzle due to the flash evaporation. In the present study, critical flow of two-phase fluids is analysized using an Isentropic-Homogeneous-Equilibrium model and a Leung model. Calculation results show that the choke of the two-phase flow can be two different types of continuous and discontinuous chokings. For the stagnation pressure below 10 Mpa it is found that the continuous choking, which is similar to the choking phenomenon of single-phase gas flow, is possible only when the degree of subcooling is less than 10K.

The Compressible flow structure behind the exit of a two-dimensional supersonic micro-nozzle (2차원 소형 초음속 노즐 하류의 압축성 유동 구조 해석)

  • Kwon, Soon-Duk;Kim, Sung-Cho;Kim, Jeong-Soo;Choi, Jong-Wook
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2006.11a
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    • pp.323-326
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    • 2006
  • This paper presents the computational results for the two-dimensional compressible non-reacted flow in a converging-diverging micro thrust nozzle of which the ratio of exit to throat width (0.541 in.) is 1.8. The RNG model is applied to calculate the turbulence by loading the standard coefficients. The results agreed very well with the experiments in the view of the shock structure and the pressure distribution at the various pressure ratios between the stagnation and the environmental states. The plume structures are also discussed on the view of the shock-cell structure.

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A Fundamental Study on the Gas Atomization of Liquid Metal (용융금속 미립화에 관한 기초적 연구)

  • Kang, Min-Sung;Choi, Jong-Youn;Kim, Heuy-Dong
    • Proceedings of the KSME Conference
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    • 2008.11b
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    • pp.2777-2781
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    • 2008
  • Gas atomization of liquid metal using nozzle technology has more advantages over other methods. Previous study shows that high-velocity gas is important for effective liquid metal atomization. An important first step towards understanding the gas atomization using nozzle is complete evaluation of the flow fields. This will provide a basis for understanding how well high velocity gas is brought to bear on the liquid metal. Present work is a fundamental study of liquid metal atomization for various pressure ratio, different gas and temperature. A two-dimension, axisymmetry compressible Navier-Stokes equations are considered. Two-equation k-epsilon turbulence model is selected.

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A Study on the Flow Characteristics of a Two - Dimensional Oblique Plate Impinging Jet (경사진 평판에서 2차원 충돌 제트의 유동 특성에 관한 연구)

  • 윤순현;김경문;김대성
    • Journal of Advanced Marine Engineering and Technology
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    • v.21 no.1
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    • pp.37-42
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    • 1997
  • Turbulent flow characteristics of a two - dimensional oblique plate impinging jet(OPIJ) were experimentally investigated. The jet mean velocity and turbulent intensity profIles were also measured along the plate. The jet Reynolds numbers(Re, based on the nozzle width)ranged from 10, 000 to 35, 000, the nozzle - to - plate distance(H/B) from 2 to 16, and the oblique angle (a) from 60 to 90 degree. It has been found that the stagnation point shifted toward the minor flow region as the oblique angle decreases and the position of the stagnation point nearly coin¬cided with that of the maximum turbulent intensity.

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Effect of Orifice Nozzle Design and Input Power on Two-Phase Flow and Mass Transfer Characteristics (2 상 유동 및 물질전달 특성에 미치는 오리피스 노즐형상과 소요동력의 영향)

  • Yang, Hei Cheon
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.40 no.4
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    • pp.237-243
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    • 2016
  • It is necessary to investigate the input power as well as the mass transfer characteristics of the aeration process in order to improve the energy efficiency of an aerobic water treatment. The objective of this study is to experimentally investigate the effect of orifice nozzle design and input power on the flow and mass transfer characteristics of a vertical two-phase flow. The mass ratio, input power, volumetric mass transfer coefficient, and mass transfer efficiency were calculated using the measured data. It was found that as the input power increases the volumetric mass transfer coefficient increases, while the mass ratio and mass transfer efficiency decrease. The mass ratio, volumetric mass transfer coefficient, and mass transfer efficiency were higher for the orifice configuration with a smaller orifice nozzle area ratio. An empirical correlation was proposed to estimate the effect of mass ratio, input power, and Froude number on the volumetric mass transfer coefficient.

Flow Measurements of Circular Jets Arrayed Circumferentially (원주상으로 배열된 원형 제트의 유동 측정)

  • Jin, Hak-Su;Kim, Sung-Cho;Kim, Jeong-Soo;Choi, Jong-Wook
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2006.11a
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    • pp.11-14
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    • 2006
  • This study investigates the flow field of multiple-jet measured by hot-wire anemometry. The experiments were classified into two cases; 6- or 7-nozzle located circumferentially in equal interval without or with a central jet. The effect of the number of nozzles the flow field was examined when the Reynolds number based on the nozzle diameter is about $10^4$. Mean Velocity, normal and Reynolds stresses were measured in the downstream of jets. The Tollmien's theory holds far downstream at 48d apart from the nozzle exit especially when a nozzle locates at the center. The general flow characteristics is influenced due to the number of nozzles.

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