• Title/Summary/Keyword: long slit

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Heat Transfer and Friction Characteristics of Slit Fin and Tube Heat Exchangers in Wet Conditions (습표면 조건에서 슬릿 핀-튜브 열교환기의 열전달 및 압력강하 특성)

  • Chang, Keun-Sun;Phan, Thanh-Long
    • Korean Journal of Air-Conditioning and Refrigeration Engineering
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    • v.19 no.1
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    • pp.1-9
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    • 2007
  • Water condensate accumulated on the surface of a fin-and-tube heat exchanger significantly affects its thermal and hydraulic performance. The purpose of this study is to investigate the effect of condensate retention on the air-side heat transfer performance and flow friction. Total 12 samples of slit and plate fin-and-tube heat exchangers with varying fin spacing and number of tube rows are tested under dry and wet conditions. The thermal fluid measurements are made using a psychometric calorimeter. Frontal air velocity varies in the range from 0.7 m/s to 1.5 m/s. Using the experimental data, presented are the heat transfer coefficients in terms of Colburn j-factor and friction factor.

An Experimental Study on Air-side Performance of Fin-and-Tube Heat Exchangers with Slit Fin

  • Chang, Keun-Sun;Phan, Thanh-Long
    • Proceedings of the SAREK Conference
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    • 2006.06a
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    • pp.627-632
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    • 2006
  • An experimental study is conducted to investigate the effect of the tube row and fin spacing on the air-side heat transfer and friction characteristics of fin-tube heat exchangers with slit fin pattern. A total of twelve samples of fin-tube heat exchangers with the nominal tube diameter of 7 mm, transverse tube pitch of 19 mm and longitudinal tube pitch of 12.5 mm are tested. The thermal fluid measurements are made using a psychometric calorimeter. The raw data are reduced to the desired heat transfer coefficient in terms of j-factor and friction factor of f for various frontal air velocities, fin pitches and number of tube rows.

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Optical Long-slit Spectroscopy of Parsec-scale Jets

  • Oh, Heeyoung;Pyo, Tae-Soo;Yuk, In-Soo;Kim, Kang-Min;Lee, Sungho;Park, Byeong-Gon
    • The Bulletin of The Korean Astronomical Society
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    • v.38 no.1
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    • pp.55.2-55.2
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    • 2013
  • We present the observational study of parsec-scale jets from YSOs reaching lengths of several arc-minutes. The medium-resolution spectroscopic data were obtained between 6000 - $7000{\AA}$ with BOAO long-slit spectrograph. By performing multi-position observation, we investigated the physical variation of the jets and the ambient gas along the whole path of the jets. The flux, electron density, ionization fraction, and electron temperature are discussed with the estimated line ratios between from [OI], [NII], $H{\alpha}$ and [SII] emission lines. This study carried out with more than 8 jets of YSOs including low- to intermediate-mass stars. We also briefly discuss the kinematics of the outflows using spatial and spectroscopic data.

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Long-slit Spectroscopy of Parsec-scale Jets from YSOs

  • Oh, Heeyoung;Pyo, Tae-Soo;Yuk, In-Soo;Park, Byeong-Gon
    • The Bulletin of The Korean Astronomical Society
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    • v.39 no.1
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    • pp.63.1-63.1
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    • 2014
  • We present a study on the parsec-scale jets from young stellar objects using long-slit spectroscopic data obtained from Bohyunsan Optical Astronomy Observatory on 2012 - 2014. Through the position-velocity diagrams, we show the radial velocity variation, peak velocity and velocity width of the outflow from several T Tauri stars and Herbig Ae/Be star. $H{\alpha}$, [OI] 6300/6363, [NII] 6548/6584 and [SII] 6716/6731 emission lines are obtained and they show various velocity features. We also compare our result with other data from literatures.

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A Study on the Performance Variation of a Three-Dimensional Hydrofoil Using Jet Flow

  • Eom, Myeong-Jin;Paik, Kwang-Jun;Lee, Ju-Han;Kang, Shin-Min;Kim, Dong-Young
    • Journal of Ocean Engineering and Technology
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    • v.35 no.1
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    • pp.24-37
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    • 2021
  • As one of the development directions of high-performance ships to reduce greenhouse gas emissions, there is research on high-performance propellers. However, in the case of conventional screw propellers, as they have been studied for a long time, there is a limit to improving efficiency only by depending on the conventional design and analysis methods. In this study, we tried to solve the problems using the Coanda effect by spraying a jet on the surface of the hydrofoil. The Coanda hydrofoil consists of a tunnel and jet slit to make jet flow. The computation was performed for each tunnel and slit position, and the efficiency according to the geometry of the hydrofoil was analyzed. In addition, a study on the 3D geometry change was conducted to analyze the performance according to the span direction spraying range and hydrofoil shape. As the height of the slit and the diameter of the tip were lower, when the slit is located in the center of the hydrofoil, the lift force increased and the drag force decreased. The increase rate of lift-to-drag ratio was different according to the shape of the hydrofoil, and the efficiency of the spraying condition of 0.1S-0.5S, which had the least effect on the vortex at the tip of the blade, was high for all 3D hydrofoils. When the geometry of the slit was optimized, and also the shape and spray range of the hydrofoil in 3D was considered, the efficiency of the jet sprayed hydrofoil was increased.

Effects of Aspect Ratio of a Fuel Injection Nozzle into a Supersonic Air Stream on Combustion Characteristics (초음속 공기유동으로의 연료 분사노즐 종횡비 변화에 대한 연소특성 연구)

  • 김경무;백승욱;김윤곤
    • Journal of the Korean Society of Propulsion Engineers
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    • v.8 no.1
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    • pp.44-53
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    • 2004
  • This paper is to investigate the combustion characteristics with a three dimensional chemical reacting flow on the aspect ratio of an exit configuration of the slit type nozzle for the fuel injection and to device the methods of combustion/mixing enhancement. The results show that both inside inflow and slit side vertices should be considered from a viewpoint of the mixing. The combustion efficiency becomes the smallest at aspect ratio, where the aspect ratio is less and more than unity, respectively. The total pressure loss becomes the largest at aspect ratio of unity due to the high penetration. All results imply that a streamwise very long slit is desirable with respect to the combustion and the pressure loss.

Probing the Starburst-AGN Connection in Type I AGN based on the 3.3 micron PAH lines

  • Woo, Jong-Hak;Kim, Ji-Hoon;Imanishi, Masatoshi
    • The Bulletin of The Korean Astronomical Society
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    • v.36 no.2
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    • pp.74.1-74.1
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    • 2011
  • To probe the connection between starburst and AGN activity, we investigate the relation between the 3.3 micron~PAH emission and AGN properties based on the new AKARI observations and the data collected from the literature. Using a sample of low-z Type I AGN, we measure the global 3.3 micron PAH luminosity from the AKARI slit-less spectroscopy. The 3.3 ${\backslash}$micron~PAH emissions are detected for 7 out of 26 target galaxies, but we find no strong correlation between the 3.3 ${\backslash}$micron~PAH emission and AGN luminosity, suggesting that global star formation may not be tightlyrelated with AGN activity. In contrast the to global star formation, the nuclear 3.3 micron~PAH emission luminosity, which are measured from ground-based long slit spectroscopy with a narrow slit, correlates with AGN luminosity. These results imply that starburst and AGN activity are directly connected at the nuclear region.

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Spectroscopic Studies of Emission Line Galaxies

  • Chun, M.S.;Y.I.Byun
    • Bulletin of the Korean Space Science Society
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    • 1993.10a
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    • pp.20-30
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    • 1993
  • Spectroscopic observations were made to study 42 emission line objects. The analysis of these long slit spectra shows that 15 out of 42 galaxies are blue compact galaxies. Among the 42 objects, 9 galaxies show the spectra of the typical starburst galaxy.

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A Study on the Flow Characteristics of the Spiral Flow Nozzle with the Width Change of Annular Slit

  • Kim, T.H.;Setoguchi, T.;Lee, Y.W.
    • Journal of the Korean Society of Visualization
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    • v.7 no.1
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    • pp.14-20
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    • 2009
  • In comparison with previous researches fur swirling flow, the spiral flow self-generated in the spiral flow nozzle has some different characteristics. It is not needed a compulsive tangential momentum to get its velocity component and has long potential core, relatively low swirl ratio, and high focusing ability. In this study, the self-generated mechanism of the spiral flow was clarified and the effect on the width of annular slit on spiral flow characteristics was investigated experimentally and numerically. As a result, the existence of tangential velocity component regardless of a compulsive angular momentum is clarified and the results obtained by experiment have a satisfactory agreement with those by numerical method, quantitatively and qualitatively.