• Title/Summary/Keyword: Impinged Jet

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Flow and Heat/Mass Transfer Characteristics of Arrays of Impingement Jets with Effusion Holes (유출홀이 설치된 배열 충돌제트의 유동 및 열전달 특성)

  • Lee, Dong-Ho;Yun, Pil-Hyeon;Jo, Hyeong-Hui
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.25 no.11
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    • pp.1606-1615
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    • 2001
  • The present study has been conducted to investigate heat/mass transfer characteristics on a target plate fur arrays of circular impingement jets with and without effusion holes. A naphthalene sublimation method is employed to determine local heat/mass transfer coefficients on the target plate. The effusion holes are located at the center of four injection holes in the injection plate where the spent air is discharged through the effusion hole after impingement on the target plate. For the array jet impingement without effusion holes, the array jets are injected into the crossflow formed by upstream spent air because the impinged jets must flow to the open exit. For small gap distances, heat/mass transfer coefficients without effusion holes are very non-uniform due to crossflow effects and re-entrainments of spent air. However, uniform distributions and enhanced values of heat/mass transfer coefficients are obtained by installing the effusion holes. For large gap distances, the crossflow has little influence on heat/mass transfer characteristics on the target palate due to the large cross-sectional open area between the injection and target plates. Therefore, the distributions and levels of heat/mass transfer coefficients are almost the same for both cases.

Development of Combined Optical System for Analysis of Impinging Butane Flame (충돌 부탄 화염의 분석을 위한 복합 광학 계측 기법 개발)

  • Baek, Seung-Hwan;Ahn, Seong-Soo;Ko, Han-Seo
    • 한국가시화정보학회:학술대회논문집
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    • 2005.12a
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    • pp.69-73
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    • 2005
  • Three-dimensional density distributions of an impinging and eccentric flame have been analyzed numerically and experimentally by a combined optical system with a digital speckle tomography. The flame has been ignited by premixed butane/air from air holes and impinged vertically against a plate located at the upper side of tile burner nozzle. In order to compare with experimental data, computer synthesized phantoms of impinging and eccentric flames have been made and reconstructed by a developed three-dimensional multiplicative algebraic reconstruction technique (MART). A new scanning technique has been developed for the analysis of speckle displacements to investigate wall jet regions of the impinging flame including sharp variation of the flow direction and pressure gradient. The reconstructed temperatures have been compared with a temperature photography by an infrared camera and results of numerical analysis using a finite-element method.

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Development of Three-dimensional Tomography Technique for Analysis of Impinging Jet (충돌 제트 분석을 위한 3차원 토모그래피 기법 개발)

  • Kim Yong-Jae;Ahn Seong Soo;Ko Han Seo
    • 한국가시화정보학회:학술대회논문집
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    • 2004.11a
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    • pp.34-35
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    • 2004
  • Three dimensional density distributions of impinging and eccentric flames have been investigated by digital speckle tomography. The flames have been ignited by a mixture of butane and air from a circular nozzle and impinged against a plate located at the upper side of the burner exit. For comparison with experimental data, computer synthesized phantoms of impinging and eccentric flames have been reconstructed by a developed three-dimensional multiplicative algebraic reconstruction technique (MART). The advanced reconstruction in the stagnation flow region involved the sharp change of the flow direction and pressure gradient has been developed using a cross-correlation method and new scanning technique for the speckle displacement.

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Prediction of sacrificial material ablation rate by corium jet impingement (노심 용융물 제트 충돌에 의한 희생물질의 침식예측)

  • Suh, Jungsoo;Kim, Hangon
    • Journal of Energy Engineering
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    • v.23 no.3
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    • pp.21-26
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    • 2014
  • EU-APR1400, the Korean nuclear reactor design for European market adopts a so-called core catcher for ex-vessel molten corium retention and cooling as a severe-accident mitigation system. Sacrificial material, which controls melt properties and modifies melt conditions favorable for corium cooling and retention, is usually employed to protect core catcher body from molten corium. Since molten corium can be ejected through a breach of a reactor pressure vessel and impinged on the sacrificial material with enhanced heat transfer at a severe accident, it is very important to predict ablation rate of sacrificial material due to corium jet impingement accurately for core catcher design. In this paper, sacrificial-material ablation model based on boundary layer theory is suggested and compared with the experimental results by KAERI.

The Spray Behavior Analysis and Space Distribution of Mixture in Transient Jet Impinging on Piston Cavity (비정상 충돌 분류의 Cavity형상에 따른 공간 농도 분포 및 거동해석)

  • Lee, S.S.;Kim, K.M.;Kim, B.G.;Chang, S.S.;Ha, J.Y.
    • Journal of ILASS-Korea
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    • v.1 no.2
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    • pp.16-23
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    • 1996
  • In case of a high-speed D.I. diesel engine. the injected fuel spray is unavoidable that the impinging on the wall of piston cavity and in this case the geometry of piston cavity has a great influence on the atomization structure and air flow fields. In the field of combustion and in many other spray applications, there are clear evidence of correlation between spray structure and emission of pollutants. Ordinary, the combustion chamber of driving engine have unsteady turbulent flow be attendant on such as the change of temperature, velocity and pressure. So the analysis of spray behavior is difficult. In this study, a single spray was impinged on each cavity wall at indicated angle in a quiescent atmosphere at room temperature and pressure, as being the simplest case, and 3 types of piston cavity such as Dish, Toroidal and Re-entrant type was tested for analyzing the influence of cavity geometry. And hot wire probe was used for analyze non-steady flow characteristics of impinging spray, and to investigate the behavior of spray, the aspects of concentration c(t), standard deviation $\sigma(t)$ and variation factor (v.f.) was measured with the lapse of time.

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Impinging Atomization of Intermittent Gasoline Sprays (간헐 가솔린 분무의 충돌에 의한 미립화 촉진)

  • 원영호;임치락
    • Transactions of the Korean Society of Automotive Engineers
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    • v.6 no.5
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    • pp.174-181
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    • 1998
  • Experimental and analytical studies are presented to characterize the break-up mechanism and atomization processes of the intermittent- impinging-type nozzle. Gasoline jets passing through the circular nozzle with the outlet diameter of 0.4mm and the injection duration of 10ms are impinged on each other. The impingement of fuel jets forms a thin liquid sheet, and the break-up of the liquid sheet produces liquid ligaments and droplets subsequently. The shape of liquid sheets was visualized at various impinging velocities and angles using the planer laser induced fluorescence (PLIF) technique. Based on the Kelvin-Helmholtz wave instability theory, the break-up length of liquid sheets and the droplet diameter are obtained by the theoretical analysis of the sheet disintegration. The mean diameter of droplet is also estimated analytically using the liquid sheet thickness at the edge and the wavelength of the fastest growing wave. The present results indicate that the theoretical results are favorably agreed with the experimental results. The size of droplets decreases after the impingement as the impinging angle or the injection pressure increase. The increment of the injection pressure is more effective than the increment of the impinging angle to reduce the size of droplets.

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Heat Transfer Characteristics of Water Jet Impinging on Oblique Surface (경사면(傾斜面)에 충돌(衝突) 하는 수분류(水噴流)의 열전달(熱傳達) 특성(特性)에 관(關)한 연구(硏究))

  • Choi, Guk-Gwang;Na, Gi-Dae;Kim, Yeun-Young;Jeon, Sung-Taek;Lee, Jong-Su
    • Solar Energy
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    • v.13 no.1
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    • pp.1-10
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    • 1993
  • The purpose of this research is to investigate the characteristics of heat transfer in the downward axisymmetric free water jet system impinged on a flat oblique plate which has the uniform heat flux. Experimental conditions considered were Reynolds number, distance between nozzle and Bat plate, inclination angle of heater surface and nozzle exit velocity. Local Nusselt number was subjected to the influence of Re number, Pr number, oblique angle of heating surface and local position of flat plate. In the wall region of downward surface, The secondary peak point of heat transfer appeared at the local point of X/D=-8 from the stagnation point. The stagnation heat transfer rate of this experimental study augments 2.4 times than that of laminar theorical solution. The stagnation nusselt number is function of Reynolds number, nozzle-plate spacing Prandtl number and oblique angle of impinging plate.

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