• 제목/요약/키워드: Film Cooling

검색결과 441건 처리시간 0.023초

로켓엔진의 막냉각 성능 예측을 위한 열설계 프로그램 개발 (Development Thermal Design Program to Predict Film Cooling Performance in Liquid Rocket Engine)

  • 조원국;문윤완;설우석
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2006년도 제26회 춘계학술대회논문집
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    • pp.161-164
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    • 2006
  • 액체로켓엔진 연소실의 막냉각 성능을 예측할 수 있는 설계프로그램을 개발하였다. 저혼합비 가스의 열차폐 효과를 전산해석으로 예측하였고 이를 기반으로 1차원 모델을 개발하여 기존의 재생냉각 설계 프로그램에 이식하였다. 문헌에 제시된 축소형 연소실에서의 막냉각 특성과 비교하여 노즐목에서의 열유속에 대한 본 프로그램의 정확성이 -16%에서 +28% 범위에 있음을 확인하였다. 연료유량의 10% 막냉각에 의하여 노즐목의 열유속을 36% 감소시킬 수 있음을 확인하였다.

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원통형과 변형된 분사홀을 갖는 터빈 블레이드의 막냉각 특성에 관한 연구 (Studies on the Film Cooling Characteristics of Turbine Blade Cylindrical and Shaped Holes)

  • 김성민;김윤제;조형희
    • 유체기계공업학회:학술대회논문집
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    • 유체기계공업학회 2001년도 유체기계 연구개발 발표회 논문집
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    • pp.334-338
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    • 2001
  • In order to investigate the effects of various injection hole shapes on the film cooling of turbine blade, three test models having cylindrical and shaped holes were used. A three-dimensional Navier-Stokes code with standard k-$\epsilon$ model was used to compute the film cooling coefficient on the film cooled turbine blade. Over 330,000 grids were used to compute the flow over the blade. Mainstream Reynolds number based on the cylinder diameter was $7.1{\times}10^4$. The turbulence intensity kept at $5.0\%$ for all inlets. The effect of coolant blowing ratio was studied for various blowing ratios. For each blowing ratios, wall temperatures around the surface of test model were calculated. Temperature was visualized using cartesian cut-cell method to obtain traces of the injected secondary air on the test surface, so we could interpret the film effectiveness as temperature distributions.

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스프레이가 분사되는 표면에서의 액막 두께 분포 측정 (Measurement of liquid film thickness distribution on sprayed surfaces)

  • 김태호;김명호;조형규;김병재
    • 한국가시화정보학회지
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    • 제21권3호
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    • pp.33-38
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    • 2023
  • Spray cooling is a method of cooling high-temperature heating elements by spraying droplets. Recently, spray cooling has been proposed for use in next-generation nuclear reactors. When droplets are sprayed onto the outer wall of a heat exchanger tube, a film boiling occurs on the outer wall. Over time, the outer wall temperature decreases, and a liquid film forms on the outer wall, and the heat exchanger outer wall is subsequently cooled by the liquid film. In this case, the liquid film thickness has a great influence on the heat removal performance. In this study, an experimental study was conducted to measure the liquid film thickness distribution in a droplet spray environment. For this purpose, a method using the electrical conductivity of the liquid was adopted.

슬롯출구 상류면의 상승과 하강에 따른 막냉각 특성 (Film Cooling Characteristics with Sunk or Lifted Upstream Wall)

  • 노석만;손창호;이근식
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2001년도 춘계학술대회논문집D
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    • pp.377-381
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    • 2001
  • Film cooling characteristics has been investigated numerically with the aid of FLUENT software for the sunk or the lifted upstream wall from the slot injection exit. In this study, with the fixed blowing ratio of 1 and the fixed coolant injection angle of $30^{\circ}$, the downstream flow field and the downstream temperature field were examined in terms of velocity vector, turbulent kinetic energy, temperature contours, and downstream wall temperature. Upstream wall was sunk or lifted from 1d to 5d(d=slot width). The result shows that the up-Id upstream wall has the best film cooling performance. This is due to the fact that the up-1d upstream wall configuration reduces velocity gradient just enough to minimize the turbulent mixing between the mainstream and the coolant just off the slot exit.

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복사냉각 시스템에서 커버의 영향 (The Experimental Study of Radiant Cooling Test System under Different Covers)

  • 변기홍
    • 설비공학논문집
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    • 제19권11호
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    • pp.797-802
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    • 2007
  • The effects of window cover on the performance of the plate type radiant cooling test system are studied. The cover materials tested are 2mm, 1mm, 0.7mm glass, Cokin 007 filter, and PVC film. The measurements are performed during the September nights of 2005 at the rooftop of the building in Seoul. The equivalent height of the building is about a building with twelve floors. The radiant cooling performance of the black painted and aluminum film coated plate are compared under no cover condition. Also the results are compared when the system has cover over the plate. In general, the covers reduce the radiant cooling temperature differences during the nighttime. Among these covers, the PVC film cover shows the best performance. In some cases, the plate with PVC film cover shows lower temperatures than the system without cover.

열 차단 필름의 적용에 따른 냉난방 부하 분석에 관한 연구 (A Study on the Analysis of Heating and Cooling Load through Applying Window Film Insulation)

  • 김석현;조영흠
    • 한국태양에너지학회 논문집
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    • 제33권6호
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    • pp.47-53
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    • 2013
  • In order to reduce the energy consumption of the building, much effort is being made. The problems are that excessive solar radiation in summer and the heat loss in winter by the increase of window area. To prevent this problems, government limited the window area ratio or the performance of windows in new buildings. In order to reduce energy consumption of the existing buildings, the window film insulation is spotlight because the window film insulation was simple to installation. This study confirmed the performance of the window film insulation and affect to heating & cooling load of buildings. The impact of the window film insulation coating was confirmed by experiment. And this study confirmed the annual heating & cooling load by simulation. As a results, the surface temperature of coated window was higher than the surface temperature of existing window. The window film insulation was increased surface temperature of window. And this study confirmed that the increased surface temperature was slightly affected the room air temperature through experiment of the insulation box. The results of the heating and cooling load by simulation, this study confirmed that the case of coated window film insulation decreased cooling load in summer and increased heating load in winter. Also the annual total heating & cooling load was increased a little in the case of coated the window film insulation.

액체로켓엔진의 막냉각에 관한 실험적 연구(I) (Experimental Study of Film Cooling in Liquid Rocket Engine(I))

  • 최영환;정해승;김유;김선진
    • 한국항공우주학회지
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    • 제33권6호
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    • pp.71-75
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    • 2005
  • 추진제로 LOX/kerosene를 사용하는 소형 액체로켓 엔진의 노즐에서 막냉각의 영향을 살펴보고자 물을 냉각제로 사용하여 로켓엔진의 노즐을 막냉각 시켰다. 막냉각제를 추력실로 흘려보내기 위한 막냉각장치를 제작하였으며, 막냉각제의 공급유량은 전체 추진제 공급 유량의 약 15~19% 하였다. 노즐의 열유속은 냉각제(물)의 온도상승과 유량을 측정하여 구하였다. 측정결과 노즐의 입구에서 막냉각제를 직접 분사시켰을 때, 노즐에서의 열유속은 크게 감소하였다.

반와류 홀의 형상 변화가 막냉각 효율에 미치는 영향 (Effects of Geometry of Anti-Vortex Holes on Film-Cooling Effectiveness)

  • 김준희;김선민;김광용
    • 한국유체기계학회 논문집
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    • 제17권2호
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    • pp.12-23
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    • 2014
  • A parametric study on anti-vortex holes for turbine blade cooling was investigated numerically. Three-dimensional Reynolds-averaged Navier-Stokes equations and shear stress transport turbulence model were used for analysis of anti-vortex film cooling. Validation of numerical results was carried out comparing with experimental data. The cooling performance of anti-vortex holes was assessed by two geometric variables, the ratio of diameters of holes and the lateral distances between the primary hole and anti-vortex hole at blowing ratios of 0.5 and 1.0. The results showed that the spatially-averaged film-cooling effectiveness increases as the ratio of the diameters increases and the distance between the primary hole and anti-vortex hole decreases.

반와류 홀의 각도가 평판의 막냉각 효율에 미치는 영향 연구 (Effect of Anti-Vortex Hole Angle on the Flat Plate Film Cooling Effectiveness)

  • 박순상;박정신;이상훈;문영기;곽재수
    • 한국유체기계학회 논문집
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    • 제17권5호
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    • pp.5-10
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    • 2014
  • In this paper, the experimental study was carried to investigate the effect of angle of the anti-vortex holes on the film cooling effectiveness on a flat plate. The pressure sensitive paint technique was applied to measure the film cooling effectiveness. Two anti-vortex hole angles of $0^{\circ}$ and $15^{\circ}$ with respect to the primary hole were considered, and the simple cylindrical hole case was also tested. The blowing ratio based on the cylindrical hole was 0.5 and the same flow rate was kept for all anti-vortex hole cases. Results showed that the film cooling effectiveness for the anti-vortex hole cases were much higher than that of the cylindrical case. Among the anti-vortex hole cases, $15^{\circ}$ angle anti-vortex hole case showed higher film cooling effectiveness than that by the $0^{\circ}$ angle anti-vortex hole case.

막냉각을 고려할 때 로켓엔진 연소실 벽면 온도변화에 대한 비정상 열해석 (Transient Thermal Analysis on Wall Temperature Change of Rocket Engine Combustion Chamber Considering Film-Cooling)

  • 하성업;이선미;문일윤;이수용
    • 한국추진공학회지
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    • 제16권5호
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    • pp.37-46
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    • 2012
  • 로켓엔진 연소실에서 막냉각을 고려한 열전달 해석을 위한 모델을 수립하였다. 연소실 내에서의 대류, 복사, 막냉각 효과는 로켓엔진을 위한 경험식을 사용하였으며, 벽 외부는 일반적인 대류, 복사 식을 적용하였다. 또한 벽 내부는 유한체적의 격자를 구성하여 시간전진법에 의해 비정상 열해석을 수행하였다. 연소압 50 기압의 액체산소/케로신 엔진을 예로 해석하였으며, 이 경우 4% 유량의 막냉각까지는 벽온도를 낮추는데 크게 기여하였으나, 그 이상의 공급은 막냉각 유량에 비해 효과가 미비함을 확인하였다.