• 제목/요약/키워드: Round jet

검색결과 82건 처리시간 0.021초

수직 상방으로 난류제트의 통계학적 특성에 관한 실험적 연구 (Experimental study of statistical characteristics of turbulent jet discharged vertically upward)

  • 이준식;이택식
    • 대한기계학회논문집
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    • 제5권4호
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    • pp.320-328
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    • 1981
  • Experimental study of a round. free air jet is accomplished using a crossed hot wire probe with a constant temperature hot wire anemometer. Mean velocity Profiles, Reynolds stresses, tubulent intensities, velocity probability densities and correlation functions are measured in the down tream region. These values are calculated and averaged inthe correlation and probability analyzer. The reults are interpreted by the output of te dual beam oscilloscope.

반원 오목면에 분사되는 제트충돌 냉각에 관한 실험적 연구 (An Experimental Study of Jet Impingement Cooling on the Semi-Circular Concave Surface)

  • 양근영;최만수;이준식
    • 대한기계학회논문집
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    • 제19권4호
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    • pp.1083-1094
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    • 1995
  • An experimental study has been carried out for jet-impingement cooling on the semi-circular concave surface. Two different nozzles(round edged nozzle and rectangular edged nozzle) are utilized and heat transfer coefficients on the concave surface have been measured under a constant heat flux condition. The characteristics of heat transfer has been discussed in conjunction with measured jet flow. Velocity and turbulence intensity of free jets issuing from two different nozzles have been measured by Laser Doppler Anemometry and theromocouple measurements have been done for temperatures on the concave surface. The effects of the nozzle shape, the distance between the nozzle exit and the stagnation point of the surface and the nozzle exit velocity on heat transfer were studied.

충돌제트의 간격변화에 따른 발열블록 표면에서의 열전달 특성에 관한 수치해석 (Numerical Analysis on the Heat Transfer Characteristics of Multiple Slot Jets at the Surface of Protruding Heated Blocks)

  • 박시우;정인기
    • Journal of Advanced Marine Engineering and Technology
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    • 제27권2호
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    • pp.229-237
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    • 2003
  • The flow and heat transfer characteristics at the surface of two-dimensional protruding heated blocks using confined impingement multiple slot jets were computationally investigated Numerical predictions were made for round-edged nozzles at several nozzle-to-target plate spacings and jet-to-jet distances, with turbulent jet Reynolds numbers ranging from 2000 to 7800. The commercial finite-volume code FLUENT was used to solve the heat transfer characteristics and flow fields using a RNG $\textsc{k}-\varepsilon$ model. The computed heat transfer characteristics at the surface of heated blocks were in good qualitative agreement with previous experimental data The results of heat transfer characteristics on the surface of protruding heated blocks are important considerations in electronics Packaging design.

완전 발달된 원형 충돌제트의 노즐 직경이 열전달에 미치는 영향 (The Effect of Nozzle Diameter on Heat Transfer to a Fully Developed Round Impinging Jet)

  • 이대희;원세열;이영민;조헌노
    • 대한기계학회논문집B
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    • 제24권4호
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    • pp.519-525
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    • 2000
  • The effect of nozzle diameter on the local Nusselt number distributions has been investigated for an axisymmetric turbulent jet impinging on the flat plate surface. The flow at the nozzle exit has a fully developed velocity profile. A uniform heat flux boundary condition at the plate surface was created using gold film Intrex. Liquid Crystal was used to measure the plate surface temperature. The experiments were made for the jet Reynolds number (Re) 23,000, the dimensionless nozzle to surface distance (L/d) from 2 to 14, and the nozzle diameter (d) from 1.36 to 3.40 cm. The results show that the Nusselt number at and near the stagnation point increase with an increasing value of the nozzle diameter.

벽면 충돌 층류 확산화염의 특성 (The characteristics of laminar diffusion flame impinging on the wall)

  • 박용열;김호영
    • 대한기계학회논문집B
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    • 제20권3호
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    • pp.979-987
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    • 1996
  • A theoretical study for the laminar round jet diffusion flame impinging on the wall was carried out to predict the characteristics and structure of impinging jet flame and heat transfer to the wall. Finite chemistry via Arrhenius equation was adopted as the combustion model. All the transport properties were considered as the variable depending on the temperature and composition. For the parametric study, the distance from nozzle to perpendicular wall and Reynolds number at nozzle exit were chosen as the major parameters. As the results of the present study, the characteristics of flow field and the distributions of temperature, density and each chemical species were obtained. The heat transfer rate from flame to the wall and the effective heating area were calculated to investigate the influence of the major parameters on the heat transfer characteristics.

450自由衝突 噴射 의 亂流流動 에 관한 實驗的 硏究 (An Experimental Study on the Turbulent Flow of a 45$^{\circ}C$ Free Cross Jet)

  • 노병준;김장권
    • 대한기계학회논문집
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    • 제8권5호
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    • pp.442-449
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    • 1984
  • 본 연구에서는 두 분류가 교우되어 배합이 이루어지는 유동역에서 3차원 방향 에 대하여 평균속도분포, 난류강도분포, 난류전단응력분포, 상관계수의 분포 및 난류 운동에너지와 운동량의 변화 등을 측정 분석하였다.

오목표면에 분사되는 경사충돌제트의 난류열전달 현상에 관한 연구 (Turbulent Heat Transfer of an Oblique Impinging Jet on a Concave Surface)

  • 임경빈;최형철;이세균;최상경;김학주
    • 설비공학논문집
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    • 제12권4호
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    • pp.371-380
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    • 2000
  • The turbulent heat transfer from a round oblique impinging jet on a concave surface were experimentally investigated. The transient measurement method using liquid crystal was used in this study. In this measurement, a preheated wall was suddenly exposed to an impinging jet while recording the response of liquid crystals to measure surface temperature. The Reynolds numbers were 11000, 23000 and 50000, nozzle-to-surface distance ratio was from 2 to 10 and the surface angles were a =$0^{\circ}\;15^{\circ},\;30^{\circ}and\;40^{\circ}$. Correlations of the stagnation point Nusselt numbers with Reynolds number, jet-to-surface distance ratio and dimensionless surface angle, which account for the surface inclined angle, are presented. The maximum Nusselt numbers, in this experiment, occurred in the direction of upstream. The displacement of the maximum Nusselt number from the stagnation point increases with increasing surface angle or decreasing nozzle-to-surface distance. In this experiment, the maximum displacement is about 0.7 times of the jet nozzle diameter when surface curvature, D/d is 10.

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횡단류 제트 와류구조의 3차원 토폴로지 (Three Dimensional Topology of Vortical Structure of a Round Jet in Cross Flow)

  • 신대식;김경천
    • 대한기계학회논문집B
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    • 제23권7호
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    • pp.918-927
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    • 1999
  • In the fully developed internal flow fields, there are complex transition flows caused by interaction of the cross flow and jet when jet is Injected Into the flow. These interactions are studied by means of the flow visualization methods. An instantaneous laser tomographic method is used to reveal the physical mechanism and the structure of vortices formation in the branch pipe flow. The velocity range of cross flow of the pipe is 0.7m/s and the corresponding Reynolds number $R_{cf}$, based on the duct height is $5.6{\times}10^3$, diameter/height ratios(d/H) 0.14 and velocity ratios 3.0. Oil mist with the size of $10{\mu}m$ diameter is used for the scattering particle. The instantaneous topological features of the vortex ring roll-up of the jet shear layer and characteristics of this flow are studied in detail by performing flow visualization in rectangular duct flow. It is found that the formation and roll-up of ring vortices is a periodic phenomenon. The detailed topology of the vortices in the near field of a cross -flow jet and the mechanism associated with them give enforced hints of vortex breakdown within the vortex system due to the interaction of the jet and the cross-flow.

온도구배를 갖는 평판에 대한 원형 충돌제트의 열전달 및 난류유동에 관한 실험적 연구 (An experimental study on the heat transfer and turbulent flow of round jet impinging the plate with temperature gradient)

  • 한충호;이계복;이충구
    • 설비공학논문집
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    • 제11권6호
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    • pp.855-860
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    • 1999
  • An experimental study of jet impingement on the surface with linear temperature gradient is conducted with the presentation of the turbulent characteristics and the heat transfer rates measured when this jet impinges normally to a flat plate. The jet Reynolds number ranges from 30,000 to 90,000, the temperature gradient of the plate is 2~$4.2^{\circ}C$/cm and the dimensionless nozzle to plate distance(H/D) is from 6 to 10. The results show that the peak of heat transfer rate occurs at the stagnation point, and the heat transfer rate decreases as the radial distance from the stagnation point increases. A remarkable feature of the heat transfer rate is the existence of the second peak. This is due to the turbulent development of the wall jet. Maximum heat transfer rate occurs when the axial distance from the nozzle to nozzle diameter(H/D) is 8. The heat transfer rate can be correlated as a power function of Prandtl number, Reynolds number and the dimensionless nozzle to plate distance(H/D). It has been found that the heat transfer rate increases with increasing turbulent intensity.

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초기조건변화에 따른 횡단류 제트 유동의 전단층와류 거동 특성 (Characteristics of Shear Layer Vortices in Crossflow Jets According to the Inlet Conditions)

  • 김경천;김상기;윤상열;이석호
    • 대한기계학회논문집B
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    • 제26권3호
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    • pp.394-401
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    • 2002
  • The instantaneous flow characteristics of a round jet issuing normally into a crossflow has been studied using a flow visualization technique and particle image velocimetry. The effects of parameters such as jet inflow profile and turbulence intensity of the jet are evaluated for various Reynolds numbers in range between 735 and 3150, which are based on the crossflow velocity and jet-pipe diameter. The jet-to-crossflow velocity ratio is fixed at the value of 3.3. Instantaneous later tomographic images of the symmetry plane of the crossflow jet show that there exist very different natures in the flow structures of the near-field of the jet even though the velocity ratio is same. It is found that when the turbulence intensity of jet is elevated, the shear layer becomes much thicker due to the strong entrainment of the ambient fluid by turbulent interaction between the jet and crossflow. The detailed characteristics of instantaneous velocity and vorticity fields are presented to illustrate the effects of the above parameters on the vertical structures of the crossflow jet.