• 제목/요약/키워드: Pressure transfer ratio

검색결과 346건 처리시간 0.027초

발포금속의 열전달 특성에 관한 실험적 연구 (Study on the Heat Transfer Characteristic of Metallic Foam)

  • 김필환;김미화;김영진;정효민;정한식
    • 대한설비공학회:학술대회논문집
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    • 대한설비공학회 2008년도 동계학술발표대회 논문집
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    • pp.618-623
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    • 2008
  • To enhancement heat transfer performance, the metallic foam as heat exchanger was studied rapidly. This was attributed to its high surface area to volume ratio as well as intensive flow mixing by tortuous flow passages. So the experimental study about the heat transfer characteristic of metallic foam is presented in this paper. The material in this experiment was used as FeCrAl which has density of 10 ppi, 20 ppi and 30 ppi respectively. And the results show the heat transfer is rise with permeability Reynolds number increase and the pressure drop metallic foam was increased with the ppi increase.

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다공판을 사용한 R-123 풀비등 열전달 촉진 (Pool Boiling Enhancement of R-123 Using Perforated Plates)

  • 김내현
    • 대한기계학회논문집B
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    • 제40권5호
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    • pp.275-281
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    • 2016
  • 본 연구에서는 비등표면 위에 다공판을 설치하여 풀비등을 촉진시키는 방안에 대하여 검토하였다. 실험은 대기압에서 R-123을 사용하여 수행되었다. 다공판은 풀비등을 현저히 촉진시켰다. 이는 다공판이 기포를 비등표면 위에 넓게 퍼뜨려 기포와 비등표면 사이 액막의 면적을 증가시키기 때문이다. 또한 높은 열유속에서는 다공도가 클수록, 낮은 열유속에서는 다공도가 작을수록 비등이 촉진되었다. 본 연구에서는 구멍 직경 2.0 mm, 구멍 간격 $2.5mm{\times}5.0mm$ 또는 $5.0mm{\times}5.0mm$, 비등 표면과의 간격 0.5 mm에서 최적 형상이 얻어졌고 이 형상들의 열전달계수는 상용 GEWA-T의 값에 근접하였다. R-123에서의 최적 다공도는 물이나 에탄올에서 보다 현저히 큰데 이는 R-123의 밀도비가 크고 증발잠열은 작기 때문이다. 한편 다공판의 비등이력은 평판보다 작았다.

승용디젤엔진 EGR 및 VGT 제어시스템의 동적특성을 고려한 Decoupler 설계 연구 (Dynamic Decoupler Design for EGR and VGT Systems in Passenger Car Diesel Engines)

  • 홍승우;박인석;손정원;선우명호
    • 한국자동차공학회논문집
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    • 제22권2호
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    • pp.182-189
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    • 2014
  • This paper proposes a decoupler design method to reduce interaction between exhaust gas recirculation (EGR) and variable geometry turbocharger (VGT) systems in passenger car diesel engines. The EGR valve and VGT vane are respectively used to control air-to-fuel ratio (AFR) of exhaust gas and intake pressure. A plant model for EGR and VGT systems is defined by a first order transfer function plus time-delay model, and the loop interaction between these systems is analyzed using a relative normalized gain array (RNGA) method. In order to deal with the loop interaction, a design method for simplified decoupler is applied to this study. Feedback control algorithms for AFR and intake pressure are composed of a compensator using PID control method and a prefilter. The proposed decoupler is evaluated through engine experiment, and the results successfully showed that the loop interaction between EGR and VGT systems can be reduced by using the proposed decoupler. Furthermore, it presents stable performance even off from the designed operating point.

실험실적 규모의 분무흡수건조반응기의 배출가스 중 아황산가스 처리성능 연구 (Flue Gas Sulfur Dioxide Removal Performance of a Bench-Scale Spray Absorption/Drying Reactor)

  • 동종인;구우회;임대현
    • 한국대기환경학회지
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    • 제12권4호
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    • pp.449-457
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    • 1996
  • The main purpose of this study was to investigate sulfur dioxide removal performance of flue gas desulfurization system utilizing a Spray Absorption/Drying Reactor. In this system, the size of droplets was considered the most significant factor and tested using a PDA system. Lime slurry flow rate, operating temperature, calcium/sulfur (Ca/S) ratio and applied air pressure were selected as major operation variables and tested/analyzed in terms of system performance. The results are as follows. 1. The $SO_2$ removal efficiencies were 49%, 74%, 85% for Ca$(OH)_2$ slurry flow rate of 10, 20, 30 ml/min, which implies that the increase of slurry flow rate improves removal efficiency. The optimum slurry flow rate in this study was, however, considered 20 ml/min because of constraints of system troubles and absorbent utilization. 2. As Ca/S ratio increased, $SO_2$ removal efficiency was observed to increase. 3. As air pressure, at the atomizing nozzole, increased from 3 to 5 $kg/cm^2, SO_2$ removal efficiency increased from 74% to 80%, because of droplet size reduction due to pressure increase during atomizing process and the increase of surface area, helping mass transfer between gas and liquid phase.

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로켓 노즐의 열전달계수 비교 연구 (Comparative Studies of Heat Transfer Coefficients for Rocket Nozzle)

  • 함희철;강윤구
    • 한국추진공학회지
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    • 제16권2호
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    • pp.42-50
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    • 2012
  • 열전달 연구의 목적은 온도와 열유속 분포를 보다 정확하게 예측하는 것이다. 이를 위해 상용 CFD 코드인 FLUENT를 사용하여 2종류의 노즐에 대해 질량유속비와 압력비를 계산하였으며, 실험결과와 잘 일치하였다. 또한 1종류의 노즐에 대해 FLUENT를 사용한 노즐 벽면에서의 열전달계수 계산결과는 노즐 축소부에서 실험결과 보다 약간 크게 예측되었으나 확대부에서는 잘 일치하고 있다. Bartz식을 이용한 열전달계수 계산결과는 전체적으로 실험결과 보다 크게 예측되었다. 계산결과가 실험결과와 차이를 보이는 원인은 노즐 내 급가속 유동에 의한 층류화, 난류모델 및 격자구성 등을 고려해 볼 수 있다.

다중 영역법을 이용한 증발식 응축관 주위의 열 및 물질전달 해석 (Numerical study of heat and mass transfer around an evaporative condenser tube by multi-zone method)

  • 윤일철;이재헌
    • 대한기계학회논문집
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    • 제19권12호
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    • pp.3317-3328
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    • 1995
  • The objective of the present study is to predict the characteristics of heat and mass transfer around an evaporative condenser. Numerical calculations have been performed using multi-zone method to investigate heat transfer rate and evaporation rate with the variation of inlet condition(velocity, relative humidity and temperature) of the moist air, the flow rate of the cooling water and the shape of the condenser tube. From the results it is found that the profile of heat flux is the same as that of evaporation rate since heat transfer along the gas-liquid interface is dominated by the transport of latent heat in association with the vaporization(evaporation) of the liquid film. The evaporation rate and heat transfer rate is increased as mass flow rate increases or relative humidity and temperature decrease respectively. But the flow rate of the cooling water hardly affect the evaporation rate and heat flux along the gas-liquid interface. The elliptic tube which the ratio of semi-minor axis to semi-major axis is 0.8 is more effective than the circular tube because the pressure drop is decreased. But the evaporation rate and heat flux shown independency on the tube shape.

회전각이 큰 터빈 동익 누설유동 영역에서의 열(물질)전달 특성 (Heat(Mass) Transfer Characteristics in the Tip-Leakage Flow Region of a High-Turning Turbine Rotor Blade)

  • 이상우;권현구
    • 대한기계학회논문집B
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    • 제28권5호
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    • pp.535-544
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    • 2004
  • The heat (mass) transfer characteristics in the tip-leakage flow region of a high-turning first-stage turbine rotor blade has been investigated by employing the naphthalene sublimation technique. The heat transfer data in the tip-leakage flow area for the tip clearance-to-span ratio, h/s, of 2.0% are compared with those in endwall three-dimensional flow region without tip clearance (h/s : 0.0 %). The result shows that the thermal load in the tip-leakage flow region for h/s = 2.0% is more severe than that in the endwall flow region for h/s : 0.0%. The thermal loads even at the leading and trailing edges for h/s = 2.0% are found larger than those for h/s = 0.0%. The tip-leakage flow results in heat transfer augmentations near the tip on both pressure and suction sides in comparison with the mid-span results.

수직 축대칭 과소팽창 충돌 제트의 표면 열전달 특성 연구 (A Study on the heat transfer characteristics of a normal axisymmetric under-expanded impinging jet on a surface)

  • 유만선;김병기;조형희;황기영;배주찬
    • 한국항공우주학회지
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    • 제33권8호
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    • pp.84-91
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    • 2005
  • 축대칭 과소팽창 수직 충돌제트에 의한 표면 열전달 특성에 대하여 실험적 연구가 진행되었다. 초음속 유동장 내부의 충격파 구조 가시화와 함께 표면에서의 압력분포 및 열전달 계수가 측정되어졌다. 표면 열전달 계수는 노즐-충돌면간 거리와 과소 팽창비에 따라서 그 경향에 차이를 보였다. 이러한 현상은 벽압력 및 충격파 가시화에 대한 결과로부터 설명할 수 있었다.

엇갈린 V-형 리브가 부착된 냉각유로에서의 열유동 수치해석 (Numerical Simulation of Flow and Heat Transfer in Cooling Channel with a Staggered V-shaped Rib)

  • 명현국;김광용
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2008년도 추계학술대회B
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    • pp.2448-2453
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    • 2008
  • The present study numerically investigates the flow and heat transfer characteristics of rib-induced secondary flow in a cooling channel with staggered V-shaped ribs, extruded on both walls. The rib-height-to-hydraulic diameter ration (h/$D_h$) is 0.17; the rib pitch-to-height ratio (p/h) equals 2.8; the Reynolds number is 50,000. Shear stress transport (SST) turbulence model is used as a turbulence closure. The present results are compared with those for a continuous V-shaped rib. Computational results show that, for average heat transfer rate the staggered V-shaped rib gives about 2.5 times higher values than the continuous V-shaped rib, while, for the streamwise pressure drop the former gives about 5 times higher values than the latter. Consequently, for the thermal performances, based on the equal pumping power condition, the staggered one gives about 2 times higher values than the continuous one. Also, for the staggered V-shaped rib, complex secondary flow patterns are generated in the duct due to the snaking flow in the streamwise direction, and more uniform heat transfer distributions are obtained.

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나프탈렌 포화공기가 분사되는 막냉각 홀을 가진 터빈 블레이드 표면의 열/물질전달 계수 측정 (Heat/Mass Transfer Measurements on a Film Cooled Blade with Naphthalene Saturated Coolant)

  • 이동현;이동호;김경민;조형희;김범수
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2010년도 제34회 춘계학술대회논문집
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    • pp.433-436
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    • 2010
  • 본 논문에서는 막냉각홀이 설치된 동익 표면에서의 열/물질전달 특성을 나프탈렌 승화법들 이용해 고찰하였다. 실험에는 저속 환형풍동이 이용되었으며, 풍동 내에는 16개의 동익으로 구성된 터빈단이 설치되어 있다. 동익의 선단부에는 막냉각을 위한 홀이 3열로 배치되어 있으며, 막냉각유체의 분사비를 1.0에서 2.0으로 조절하며 국소 열/물질전달계수를 측정하였다. 전반적인 열/물질전달 계수는 분사비가 높아짐에 따라 증가하며, 박리기포에 의해 압력면에 형성된 낮은 열/물질전달 계수를 갖는 영역은 분사비의 증가와 함께 사라진다.

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