• Title/Summary/Keyword: Jet Temperature

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미세 원형 충돌수제트의 부분 대류비등에 있어서 자유표면/잠입 제트의 국소 열전달 특성 (Local Heat Transfer Characteristics in Convective Partial Boiling by Impingement of Free-Surface/Submerged Circular Water Jets)

  • 조형희;우성제;신창환
    • 설비공학논문집
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    • 제14권6호
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    • pp.441-449
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    • 2002
  • Single-phase convection and partial nucleate boiling in free-surface and submerged jet impingements of subcooled water ejected through a 2-mm-diameter circular pipe nozzle were investigated by local measurements. Effects of jet velocity and nozzle-to-imping-ing surface distance as well as heat flux on distributions of wall temperature and heat transfer coefficients were considered. Incipience of boiling began from far downstream in contrast with the cases of the planar water jets of high Reynolds numbers. Heat flux increase and velocity decrease reduced the temperature difference between stagnation and far downstream regions with the increasing influence of boiling in partial boiling regime. The chance in nozzle-to-impinging surface distance from H/d=1 to 12 had a significant effect on heat transfer around the stagnation point of the submerged jet, but not for the free-surface jet. The submerged jet provided the lower cooling performance than the free-surface jet due to the entrainment of the pool fluid of which temperature increased.

피스톤 헤드 온도에 오일 제트가 미치는 영향에 대한 연구 (Study of Oil Jet Effect on the Temperature of Piston Head)

  • 민선기
    • 한국산학기술학회논문지
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    • 제19권11호
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    • pp.536-540
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    • 2018
  • 엔진의 성능이 향상될수록 엔진 내부에서 연소되는 연료의 양이 증가하고 그에 따라 엔진의 온도는 증가하게 된다. 특히 피스톤 헤드의 경우 냉각이 어려우므로 피스톤 헤드의 온도가 높아지게 된다. 그러나 피스톤 헤드의 온도가 너무 높게 되면 피스톤 헤드 표면에서 이상 연소가 발생하기 쉬워 토크 저하 및 엔진 파손과 같은 결과를 가져온다. 피스톤 헤드의 온도를 낮게 하기 위하여 오일을 피스톤 헤드 하단부로 분사하는 오일 제트가 사용되는데, 본 연구에서는 오일 제트에 의한 피스톤 헤드 냉각 효과를 확인하기 위하여 템플러그를 사용하여 엔진 작동시 피스톤 헤드의 온도를 측정하였다. 템플러그는 일종의 센서로 피스톤 헤드의 온도에 따라 템플러그의 경도가 변화하여 변화된 경도를 이용하여 피스톤 헤드의 온도를 측정한다. 템플러그를 사용하여 피스톤 헤드의 최고 온도를 오일 제트가 없는 상태와 설치된 상태에서 측정하였다. 오일 제트가 설치됨에 따라 피스톤 헤드의 온도는 변화되었다. 최고 온도 부위가 중앙부위에서 전후부위로 변경되었다. 또한 피스톤 헤드 내에서 온도 편차가 감소하여 좀 더 균일한 피스톤 헤드 온도 분포를 얻을 수 있었다.

냉각수 온도에 따른 수분류 충돌제트의 열전달 특성 연구 (Effect of Cooling Water Temperature on Heat Transfer Characteristics of Water Impinging Jet)

  • 이정호;유청환;도규형
    • 열처리공학회지
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    • 제23권5호
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    • pp.249-256
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    • 2010
  • Water jet impingement cooling has been widely used in a various engineering applications; especially in cooling of hot steel plate of steelmaking processes and heat treatment in hot metals as an effective method of removing high heat flux. The effects of cooling water temperature on water jet impingement cooling are primarily investigated for hot steel plate cooling applications in this study. The local heat flux measurements are introduced by a novel experimental technique that has a function of high-temperature heat flux gauge in which test block assemblies are used to measure the heat flux distribution during water jet impingement cooling. The experiments are performed at fixed flow rate and fixed nozzle-to-target spacing. The results show that effects of cooling water temperature on the characteristics of jet impingement heat transfer are presented for five different water temperatures ranged from 5 to $45^{\circ}C$. The local heat flux curves and heat transfer coefficients are also provided with respect to different boiling regimes.

동축류 제트에서 초기 온도 변화에 따른 난류 부상화염 특성 (Characteristics of Turbulent Lifted Flames in Coflow Jet with Initial Temperature Variations)

  • 김길남;원상희;정석호
    • 한국연소학회:학술대회논문집
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    • 한국연소학회 2004년도 제28회 KOSCO SYMPOSIUM 논문집
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    • pp.15-20
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    • 2004
  • Characteristics of turbulent lifted flames in coflow jet have been investigated by varying initial temperature through the heating of coflow air. In the turbulent regime, liftoff height increases linearly with fuel jet velocity and decreases nonlinearly as the coflow temperature increases. This can be attributed to the increase of turbulent propagation speed, which is strongly related to laminar burning velocity. Dimensionless liftoff heights are correlated well with dimensionless jet velocity, which are scaled with parameters determining local flow velocity and turbulent propagation speed. This implies that the turbulent lifted flames are stabilized by balance mechanism between local turbulent burning velocity and flow velocity. Blowout velocity can be obtained from the ratio of mixing time to chemical time. Comparing to previous researches, thermal diffusivity should be evaluated from the initial temperature instead of adiabatic flame temperature.

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분광학적 방법에 의한 Plasma Jet의 온도분석 측정 (Spectroscopic Measurement of Temperature Distribution in Some Plasma Jets)

  • 전춘생;박용관;임명선
    • 전기의세계
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    • 제26권2호
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    • pp.104-110
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    • 1977
  • This paper investigates temperature distribution of plasma jets which used argon gas, and nitrogen gas mixed with argon as working fluids in spectroscopic method, and studies correlations between them main results are as follows; 1) The temperature at the center of plasma jet increases with are current and gas flow, and decreases with magnetic flux density along the axial direction. 2) The changing rate of temperature of plasma jet in the radial direction decreases rapidly beyond 2mm from central axis. 3) Temperature drop rate of plasma jet in the central axis direction appears most apparant beyond 13mm above the nozzle exit. 4) When argon gas mixed with a small amount of nitrogen, plasma temperature increases at same are current compared with the case of argon gas only.

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동축류 제트에서 초기 온도 변화에 따른 난류 부상화염 특성 (Characteristics of Turbulent Lifted Flames in Coflow Jet with Initial Temperature Variations)

  • 김길남;원상희;정석호
    • 한국연소학회지
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    • 제9권1호
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    • pp.32-38
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    • 2004
  • Characteristics of turbulent lifted flames in coflow jet have been investigated by varying initial temperature through the heating coflow air. In the turbulent regime, liftoff height increases linearly with fuel jet velocity and decreases nonlinearly as the coflow temperature increases. This can be attributed to the increase of turbulent propagation speed, which is strongly related to laminar burning velocity. Dimensionless liftoff heights are correlated well with dimensionless jet velocity, which are scaled with parameters determining local flow velocity and turbulent propagation speed. This implies that the turbulent lifted flames are stabilized by balance mechanism between local turbulent burning velocity and flow velocity. Blowout velocity can be obtained from the ratio of mixing time to chemical time. Comparing to previous researches, thermal diffusivity should be evaluated from the initial temperature instead of adiabatic flame temperature.

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온도와 압력의 변화에 따른 석유계 및 바이오항공유의 점화특성 분석 (Ignition Characteristics of Petroleum-based and Bio Aviation Fuel According to the Change of Temperature and Pressure)

  • 강샛별
    • 청정기술
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    • 제25권3호
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    • pp.238-244
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    • 2019
  • 본 연구에서는 온도와 압력의 변화에 따른 석유계항공유(Jet A-1), 바이오항공유(Bio-6308) 그리고 두 항공유를 50:50 (v:v)으로 혼합한 연료의 점화특성의 변화에 대한 분석을 수행하였다. Combustion research unit (CRU) 장비를 사용하여 각 항공유의 점화지연시간을 측정하였으며, GC/MS 및 GC/FID를 사용하여 각 항공유를 구성하는 화합물에 대한 정성 및 정량적인 분석을 수행하였다. 그 결과, 모든 연료의 경우에서 온도와 압력이 증가할수록 점화지연시간이 짧게 측정 되었으며, 특히 압력보다 온도의 영향을 더 많이 받는 것을 확인하였다. 또한, 모든 측정 조건에서 Jet A-1의 점화지연시간이 가장 길게 측정되었는데 이는 Jet A-1을 약 22.48%의 비율로 구성하는 방향족화합물이 산화되는 과정에서 생성되는 benzyl radical이 구조적으로 매우 안정한 특성을 갖기 때문인 것으로 판단되었다. 이러한 benzyl radical은 negative temperature coefficient (NTC) 구간에 영향을 줄 수 있는 반응을 억제하여, Jet A-1의 경우에서는 온도가 증가함에 따라 점화지연시간이 짧아지는 정도가 감소하는 구간이 없는 것을 확인하였다. Jet A-1과 Bio-6308을 50:50 (v:v)으로 혼합한 연료의 점화특성은 Bio-6308 보다는 Jet A-1과 비슷한 경향을 나타내는 것을 통해 기존의 시스템을 변경하지 않고서도 실제로 적용이 가능함을 확인하였다.

스팀분사 세탁시스템의 세탁효율 분석 (Washing Efficiency of Steam Jet Washing Process)

  • 서문호;이아진;정수현;양승도;김형섭;고준석
    • 한국염색가공학회지
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    • 제18권6호
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    • pp.69-79
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    • 2006
  • The washing characteristics of steam jet heating process have been compared with other washing processes, such as low temperature process(standard process, below $40^{\circ}C$) and high temperature process(boiling process, up to $95^{\circ}C$) with the standard soil fabric, EPMA 105. Steam jet heating process showed almost the same washing efficiency as high maximum temperature process for pig's blood and wine. This result can be explained with the higher surface temperature of washing materials in steam jet process compared with direct boiling process. In terms of the energy and water consumption, the steam jet washing process showed significant savings compared with direct boiling type washing process.

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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가스절단용 초음속 제트유동에 관한 기초적 연구 (A Fundamental Study of Supersonic Coaxial Jets for Gas Cutting)

  • 이권희;구병수;김희동
    • 대한기계학회논문집B
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    • 제25권6호
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    • pp.837-844
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    • 2001
  • Jet cutting technology currently makes use of a generic supersonic gas jet to improve the cutting speed and performance. In order to get a better understanding of the flow characteristics involved in the supersonic jet cutting technology, the axisymmetric Navier-Stokes equations have been solved using a fully implicit finite volume method. Computations have been conducted to investigate some major characteristics of supersonic coaxial turbulent jets. An assistant gas jet has been imposed on the primary gas jet to simulate realistic jet cutting circumstance. The pressure and the temperature ratios of the primary and assistant gas jets are altered to investigate the major characteristics of the coaxial jets. The total pressure and Mach number distributions, shock wave systems, and the jet core length which characterize the coaxial jet flows are strongly affected by the pressure ratio, but not significantly dependent on the total temperature ratio. The assistant gas jet greatly affects the basic flow characteristics of the shock system and the core length of under and over-expanded jets.