• Title/Summary/Keyword: 공기측 입구속도

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A Study on Flow Characteristics of Developing Laminar Pulsating Flows in a Square Duct (정4각단면덕트 입구영역에서 층류맥동유동 유동특성에 관한 연구)

  • 박길문
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.15 no.5
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    • pp.1683-1696
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    • 1991
  • 본 연구에서는 정4각단면덕트 입구영역에서 층류맥동유동(laminar pulsating flows)의 유동특성을 이론 및 실험적으로 규명하기 위하여, 이론적 방법으로 덕트 입 구영역에서의 층류맥동유동에 대한 운동량방정식을 유도한 후 비선형인 대류항을 선형 화 시켜서 라플라스변환으로 속도분포식의 해를 구하였고, 실험적인 방법으로는 시험 덕트 크기는 횡단면의 가로*세로가 40mm*40mm이고, 길이가 4000mm인 정4각단면덕트 입구영역에서 송풍기에 의한 공기흡입유동으로 층류진동유동을 발생하며 이들 두유동 을 합성시켜 발생한 층류맥동유동에 대하여 열선유속계의 열선신호로부터 얻어진 속도 파형을 고찰하여 덕트내의 맥동유동에 대한 임계레이놀즈수를 결정하고 속도분포를 측 정하였다. 그리고 이론적으로 얻어진 속도분포식과 열선유속계로 측정한 속도분포를 비교검토하여 정확성을 검증하고, 이들 해석결과로 부터 층류맥동유동의 입구길이(en- trance lenght)식을 결정하여 제안하였다.

A study on the performance of the finned tube heat exchanger affected by the frosting using CFD tool (전산해석을 이용한 착상이 핀튜브 열교환기 성능에 미치는 영향에 관한 연구)

  • Kim, Sung-Jool;Choi, Ho-Jin;Ha, Man-Yeong;Bang, Seon-Wook
    • Proceedings of the KSME Conference
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    • 2008.11b
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    • pp.2738-2743
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    • 2008
  • We conducted a study by computational simulation about the effects of frost thickness on the pressure drop and heat transfer characteristics as whole heat exchanger configuration changes. In order to perform the analysis for validation, we assumed that frost properties have constant values and the frost layers that are formed on the fin and tube surfaces are uniform. In order to find the constant thermal conductivity of frost layer, a variety of frost thermal conductivities are performed in our work and compared with the results by Lee et al. [4] and Yang et al. [5] proposed many experimental data about the 2-rows and 2-columns finned tube heat exchanger. The numerical results agreed well with the experimental data when frost conductivity is 0.07W/mK. After the validation had performed, we applied this procedure to the finned tube heat exchanger of domestic refrigeration and investigated the thermo-hydraulic characteristic of the heat exchanger affected by frost thickness according to the inlet velocities and temperatures of air considering the configuration change such as fin pitch.

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기체 방사성물질 제거용 활성탑 내에서의 유속분포 결정시험

  • 강덕원
    • Proceedings of the Korean Nuclear Society Conference
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    • 1996.05d
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    • pp.88-94
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    • 1996
  • 원자력발전소의 공조계통에 설치되어 운영되는 기체 방사성물질 제거용 첨착 활성탄 탑내에서 균일한 공기 유속분포가 유지되고 있는지를 확인하기 위한 실험을 실시하였다. 본 실험에 사용되는 장비(Tester for Flow Distribution, 이하 TFD라 함)는 원자력발전소에서 사용하는 첨착 활성탄 필터(Adsorber)내의 흡착층을 모방하여 자체에서 제작하였으며, 시험조건들은 실제의 값을 기준으로 적용하였다. 각 위치에서의 보정된 용적 유속을 구하기 위해 자체에서 만든 "FLOWD"라는 계산프로그램을 사용하였으며, 입구 및 출구측 공간에 10" 간격으로 각 6개씩 유속 감지기를 설치하여 면속도를 구하였다. 각 지점에서의 면속도는 평균 0.24449m/s로 각 구간에서의 겉보기 면속도의 분포는 매우 균일한 값을 나타내었으며, 약 2% 이내의 편차로 활성탄 탑내에서의 공기의 흐름이 균일하게 통과함을 확인할 수 있었다.통과함을 확인할 수 있었다.

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Comparison of Heat Transfer Performance and Pressure Drop of Fin-Tube and Aluminum Heat Exchangers (핀-튜브 열교환기와 알루미늄 열교환기의 전열성능과 압력강하 특성비교)

  • Chang, Keun-Sun;Lee, Hyun-Su;Kim, Jae-Duck
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.10 no.2
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    • pp.222-229
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    • 2009
  • This study presents comparison of heat transfer and air side friction characteristics in a condenser condition of air conditioner between Louver fin-tube heat exchangers and aluminum parallel heat exchangers. All experiments are performed using an air-enthalpy type calorimeter, which is designed based on the method described in ASHRAE standards. The air velocities crossing the heat exchanger tubes are varied from 0.7 to 1.6 m/s with 0.3 m/s interval, maintaining air dry temperature and relative humidity at $20^{\circ}C$ and 60% respectively. Water temperature and flow rate inside the tube are $70^{\circ}C$ and 10 LPM, respectively. Experimental results show that the heat transfer performances of aluminum heat exchangers are 17-163% higher than those of Louver fin-tube heat exchangers based on the data per unit volume, mass, and heat transfer area, whereas air side pressure drops of aluminum heat exchangers are 19-81% lower.

Numerical Modeling of Current Density and Water Behavior at a Designated Cross Section of the Gas Diffusion Layer in a Proton Exchange Membrane Fuel Cell (고분자전해질 연료전지의 동작압력에 대한 가스 확산층의 위치 별 전류밀도 및 수분거동에 대한 수치해석)

  • Kang, Sin-Jo;Kim, Young-Bae
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.36 no.2
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    • pp.161-170
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    • 2012
  • There are many factors to consider when attempting to improve the efficiency of fuel cell operation, such as the operation temperature, humidity, stoichiometry, operation pressure, geometric features, etc. In this paper, the effects of the operation pressure were investigated to find the current density and water saturation behavior on a cross section designated by the design geometry. A two-dimensional geometric model was established with a gas channel that can provide $H_2$ to the anode and $O_2$ and water vapor to the cathode gas diffusion layer (GDL). The results from this numerical modeling revealed that higher operation pressures would produce a higher current density than lower ones, and the water saturation behavior was different at operation pressures of 2 atm and 3 atm in the cathode GDL. In particular, the water saturation ratios are higher directly below the collector than in other areas. In addition, this paper presents the dependence of the velocity behavior in the cathode on pressure changes, and the velocity fluctuations through the GDL are higher in the output area than in inlet area. This conclusion will be utilized to design more efficient fuel cell modeling of real fuel cell operation.

A Study on Heat Transfer and Pressure Drop Characteristics of Staggered Tube Banks using CFD Analysis (CFD해석을 통한 엇갈린형 관군의 열전달 및 압력강하 특성에 관한 연구)

  • Zhao, Liu;Yoon, Jun-Kyu
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.16 no.5
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    • pp.2985-2992
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    • 2015
  • In this study, the characteristics of heat transfer and pressure drop was theoretically analyzed by changing longitudinal pitch, bump phase, location of vortex generator about the staggered tube banks by applying SST (Shear Stress Transport) turbulence model of ANSYS FLUENT v.14. Before carrying out CFD (Computational Fluid Dynamics) analysis, It is presumed that the boundary condition is the tube surface temperature of 363 K, the inlet air temperature of 313 K and the inlet air velocity of 5-10 m/s. The results indicated that the heat transfer coefficient is not affected by the longitudinal pitch and the bump phase of circle type was more appropriate than serrated type in the characteristics of heat transfer and pressure drop. Additionally, in case of vortex generator location, the heat transfer characteristics showed that forward location of tube was more favorable 4.6% than backward location.

A study on heat transfer and pressure drop characteristics of plain fin-tube heat exchanger using CFD analysis (CFD 해석을 통한 Plain형 핀-튜브 열교환기의 열전달 및 압력강하 특성에 관한 연구)

  • Liu, Zhao;Yoon, Jun-Kyu
    • Journal of Advanced Marine Engineering and Technology
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    • v.38 no.6
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    • pp.615-624
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    • 2014
  • The fin-tube heat exchanger being used for industrial boiler, radiator, refrigerator has been conducted in various studies to improve it's performance. In this study, the characteristics of heat transfer and pressure drop was theoretically analyzed according to longitudinal pitch, location of vortex generator, bump phase and number of the tube surface about the plain fin-tube heat exchanger. The boundary condition for the CFD (Computational Fluid Dynamics) analysis applied with the SST (Shear Stress Transport) turbulence model assumed as the tube surface temperature of 333 K, the inlet air temperature of 423-438 K and the inlet air velocity of 1.5~2.1 m/s. The analysis results indicated that the heat transfer coefficient is not affected highly by the longitudinal pitch, and the heat transfer characteristics was more favorable when the vortex generator was located in front of the tube. Also the bump phase of the tube surface indicated that circle type was more appropriate than serrated type and triangle type in the characteristics of heat transfer and pressure drop, and the sixteen's bump phase of circle type was most favorable.