• 제목/요약/키워드: Naphthalene sublimation technique

검색결과 88건 처리시간 0.025초

열전달과 물질전달의 유사성에 관한 연구 (A study on the Analogy between Heat Transfer and Mass Transfer)

  • 유성연;노종광;정문기
    • 대한기계학회논문집
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    • 제17권10호
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    • pp.2624-2633
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    • 1993
  • Mass transfer experiment by naphthalene sublimation method has great advantages in measurement of local transfer coefficients in the region of a three dimensional flow or for a model of complex geometry, which is considered to be very difficult with conventional heat transfer measurements. Mass transfer data obtained by naphthalene sublimation technique are converted to the heat transfer data through heat/mass transfer analogy. This analogy is valid for a simple or laminar flow, but new insight is needed when applying to a turbulent flow or complex flow such as separation, reattachment and recirculation, The purpose of this research is to investigate how geometries and flow conditions incorporate heat/mass transfer analogy. Mass transfer experiments are performed using naphthalene sublimation technique for a flat plate, a circular cylinder, and rectangular cylinders. And mass transfer data are compared with earlier heat transfer measurements for the same geometries. Usefulness of analogy relation between heat and mass transfer is examined with these results.

나프탈렌승화법을 이용한 사각관 주위에서의 물질전달에 관한 연구 (A Study on the Mass Transfer from a Square Cylinder Using Naphthalene Sublimation Technique)

  • 유성연
    • 대한기계학회논문집
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    • 제14권5호
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    • pp.1300-1310
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    • 1990
  • 본 연구에서는 양각과 레이놀즈수를 변화시켜 가면서 사각관 각 면에서의 국 소물질전닭계수를 측정하여, 유동의 정체, 가속, 박리, 재부착, 와류유출등의 복잡한 유동현상이 물질전달에 미치는 영향을 고찰하고자 한다. 한편 Igarashi의 열전달 측 정 결과와 비교하여 열전달과 물질전달의 유사성을 고찰하고, 복잡한 유동이나 3차원 유동영역에서의 열전달해석에 나프탈렌승화법을 이용한 물질전달실험의 응용 가능성을 검토하고자 한다.

큰 회전각을 가지는 터빈 블레이드 표면에서 나프탈렌승화법을 이용한 열(물질)전달계수 측정 (Measurements of Heat (Mass) Transfer Coefficient on the Surface of a Turbine Blade with n High Turning Angle Using Naphthalene Sublimation Technique)

  • 권현구;이상우;박병규
    • 대한기계학회논문집B
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    • 제26권8호
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    • pp.1077-1087
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    • 2002
  • The heat (mass) transfer characteristics on the blade surface of a high-turning first-stage turbine rotor for power generation has been investigated by employing the naphthalene sublimation technique. A four-axis profile measurement system is developed successfully for the measurements of local sublimation depth on the curved surface In the leading edge region, there is a good agreement between the present heat (mass) transfer data and the previous result on a turbine blade with a moderate turning angle, but some discrepancies are found in the mid-chord heat (mass) transfer between the two results. The local heat (mass) transfer on the present suction surface is greatly enhanced due to an earlier boundary transition, compared with that on a turbine blade with a moderate turning angle, meanwhile there is only a slight change in the pressure-side heat (mass) transfer between the two different turbine rotors. In general, the heat (mass) transfer augmentation by the endwall vortices is found much higher on the suction surface than on the pressure surface.

나프탈렌승화법을 이용한 터빈 익렬 끝벽에서의 열(물질)전달계수 측정 (Measurements of Endwall Heat(Mass) Transfer Coefficient in a Linear Turbine Cascade Using Naphthalene Sublimation Technique)

  • 이상우;전상배;박병규
    • 대한기계학회논문집B
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    • 제25권3호
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    • pp.356-365
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    • 2001
  • Heat (mass) transfer characteristics have been investigated on the endwall of a large-scale linear turbine cascade. Its profile is based on the mid-span of the first-stage rotor blade in a industrial gas turbine. By using the naphthalene sublimation technique, local heat (mass) transfer coefficients are measured for two different free-stream turbulence intensities of 1.3% and 4.7%. The results show that local heat (mass) transfer Stanton number is widely varied on the endwall, and its distribution depends strongly on the three-dimensional vortical flows such as horseshoe vortices, passage vortex, and corner vortices. From this experiment, severe heat loads are found on the endwall near the blade suction side as well as near the leading and trailing edges of the blade. In addition, the effect of the free-stream turbulence on the heat (mass) transfer is also discussed in detail.

A Naphthalene Sublimation Study on Heat/Mass Transfer for Flow over a Flat Plate

  • Park, Jong-Hark;Yoo, Seong-Yeon
    • Journal of Mechanical Science and Technology
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    • 제18권7호
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    • pp.1258-1266
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    • 2004
  • It is important to completely understand heat/mass transfer from a flat plate because it is a basic element of heat/mass transfer. In the present study, local heat/mass transfer coefficient is obtained for two flow conditions to investigate the effect of boundary layer using the naphthalene sublimation technique. Obtained local heat/mass transfer coefficient is converted to dimensionless parameters such as Sherwood number, Stanton number and Colburn j-factor. These also are compared with correlations of laminar and turbulent heat/mass transfer from a flat plate. According to experimental results, local Sherwood number and local Stanton number are in much better agreement with the correlation of turbulent region rather than laminar region, which means analogy between heat/mass transfer and momentum transfer is more suitable for turbulent boundary layer. But average Sherwood number and average Colburn j-factor representing analogy between heat/mass transfer and momentum transfer are consistent with the correlation of laminar boundary layer as well as turbulent boundary layer.

4-축 나프탈렌 승화깊이 측정시스템을 이용한 터빈 블레이드 표면에서의 열(물질)전달계수 측정 (Measurement of Heat (Mass) Transfer Coefficient on the Blade Surfaces of a Linear Turbine Rotor Cascade With a Four-Axis Naphthalene Profile Measuring System)

  • 권현구;이상우;박병규
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2001년도 추계학술대회논문집B
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    • pp.42-47
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    • 2001
  • The heat (mass) transfer characteristics on the blade surface of a first-stage turbine rotor cascade for power generation has been investigated by employing the naphthalene sublimation technique. A four-axis profile measurement system is successfully developed for the measurements of the local heat (mass) transfer coefficient on the curved blade surface. The experiment is carried out at the free-stream Reynolds number and turbulence intensity of $2.09\times10^5$ and 1.2%. The results on the blade surfaces show that the local heat (mass) transfer on the suction surface is strongly influenced by the endwall vortices, but that on the pressure surface shows a nearly two-dimensional nature. The pressure surface has a more uniform distribution of heat load than the suction one.

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다환 방향족 탄화수소(PAH) 분해 미생물 탐색을 위한 승화법의 개발 (Application of a Modified Sublimation Method to Screen for PAH-Degrading Microorganisms)

  • 권태형;김준태;김종식
    • 미생물학회지
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    • 제46권1호
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    • pp.109-111
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    • 2010
  • 다환 방향족 탄화수소(PAH; polycyclic aromatic hydrocarbon)는 발암성, 돌연변이 유발성, 유전독성을 지니기 때문에 인체위해성이 큰 물질로 알려져 있다. 기존 PAH 분해 미생물 탐색 방법중 독성이 강한 유기용매에 PAH를 용해시켜 미생물에 직접 분무하는 분무법, 미생물과 직접 혼합하는 한천중층법은 미생물 생장에 영향을 줄 뿐만 아니라, 특히 많이 쓰이는 분무법의 경우 분무되는 PAH의 양을 조절하기가 어렵고 멸균상태를 유지하기가 힘들다는 단점이 있다. 그래서 본 논문에서는 이와 같은 단점을 보완한 방법으로 승화법(Alley, Jeremy F. and Lewis R. Brown. 2000. Use of sublimation to prepare solid microbial media with water-insoluble substrates. Appl. Environ. Microbiol. 66, 439-442)을 도입하여 적용하였다. 그 결과 상용휘발유 및 태안유류유출지 시료로부터 분리한 350분리균주 중에서 7균주가 단일 PAH 또는 복수의 PAH 분해에 관여했다. 특히 Corynebacterium sp. SK20, Rhodococcus sp. TA24, Streptomyces sp. TA27은 시험한 pyene, phenanthrene, naphthalene에, Gordonia sp. H37는 pyrene, naphthalene에, Arthrobacter sp. S49는, naphthalene, phenanthrene에 활성이 있었다.

Plate fin-oval tube 열교환기에서 와류발생체에 의한 fin 표면에서의 국소 열전달 특성 (Local Heat Transfer Characteristics on Fin Surface of Plate Fin - Oval Tube with Delta Wing Vortex Generators)

  • 신석원;정인기;김수연
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2007년도 춘계학술대회B
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    • pp.2390-2395
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    • 2007
  • The present research was experimentally performed to analyze the effect of delta-wing vortex generators(DWVG) on the heat transfer of fin surface of the plate fin-oval tube. The local heat transfer coefficient of the fin surface for four kinds of DWVG's arrangement was measured by the naphthalene sublimation technique for Reynolds numbers ranging from 2000 to 3200. The results showed that the heat transfer of the plate fin-oval tube can be significantly enhanced by DWVG for relatively low Reynolds numbers.

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노즐형상에 따른 돌출 발열블록표면에서의 충돌분류 열전달 특성 (Effect of nozzle geometry on the jet impingement heat transfer characteristics at protruding heated blocks)

  • 정인기;박시우
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2000년도 추계학술대회논문집B
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    • pp.93-98
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    • 2000
  • An experimental investigation on heat transfer characteristics of two-dimensional heated blocks using a confined impinging slot jet has been performed. At p/w=1, the effects of jet Reynolds number($Re=3900{\sim}12000$), dimensionless nozzle to block distance(H/B=1, 2, 4, 6) and nozzle type have been examined with five isothermally heated blocks. With the measurement of jet mean velocity and turbulence intensity distributions at nozzle exit, initially turbulent regimes, are classified. To clarify local heat transfer characteristics, naphthalene sublimation technique were used. The local and average heat transfer of heated blocks increase with the sharp-edged nozzle and increasing jet Reynolds number.

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사각봉이 배열된 슬롯제트 충돌면에서 노즐형상이 열전달에 미치는 영향 (Effect of nozzle geometry on heat transfer of confined slot jet impingement on a flat plate with square rods)

  • 정인기;박시우;고완욱
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2000년도 추계학술대회논문집B
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    • pp.272-277
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    • 2000
  • The heat transfer characteristics of confined turbulent slot jet impingement on the flat plate with square rods(turbulence promoter) have been experimentally investigated at different nozzle configuration. The effects of jet Reynolds number (Re=3900, 5800, 7800, 9700), dimensionless slot-to-plate distance(H/B=4, 6, 8) and clearance(c) between square rods and the plate were examined. Measurement of heat transfer rate were conducted using naphthalene sublimation technique. When square rods were inserted over the heat transfer surface, heat transfer rate was slightly increased in the wall jet region and the sharp-edged orifice nozzle was heigher than squared orifice nozzle.

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