• 제목/요약/키워드: $k-\varepsilon$ model

검색결과 750건 처리시간 0.021초

미세버블펌프 수치모델평가 및 검증 (Evaluation for the Numerical Model of a Micro-Bubble Pump)

  • 이상문;장춘만
    • 한국수소및신에너지학회논문집
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    • 제27권1호
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    • pp.121-126
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    • 2016
  • Hydraulic performance of a micro-bubble pump has been analyzed by numerical simulation and experimental measurements. Flow recirculation apparatus between the pump inlet and outlet reserviors has been adopted to measure pump performance according to flow conditions sequentially. To analyze three-dimensional flow field in the micro-bubble pump, general analysis code, CFX, is employed. SST turbulence model is employed to estimate the eddy viscosity and compared the pump performance to k-${\varepsilon}$ model. Unstructured grids are used to represent a composite grid system including blade, casing and inlet casing. It is found that the numerical model used in the present study is effective to evaluate the pump performance. From the numerical simulation, low velocity region due to pressure loss is decreased where pump efficiency has maximum value. Detailed flow field inside the micro-bubble pump is also analyzed and compared.

유적 합체기가 포함된 공기-물-기름 분리 공정에 대한 3상 Eulerian 전산유체역학 (Three-Phase Eulerian Computational Fluid Dynamics (CFD) of Air-Water-Oil Separator with Coalescer)

  • 임영일;;박치균;이병돈;김병국;임동하
    • Korean Chemical Engineering Research
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    • 제55권2호
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    • pp.201-213
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    • 2017
  • 물이 포함된 원유는 oil separator 를 거쳐 물이 제거된다. 본 연구의 목적은 공기-물-기름 3상 혼합물에 대한 3차원 oil separator 의 분리성능을 예측하기 위하여 Eulerian 전산유체역학(CFD: computational fluid dynamics) 모델을 개발하는 것이다. 비압축성, 등온, 비정상상태 CFD 모델식은 공기상을 연속상으로, 물과 기름상을 분산상으로 정의하며, 운동량 보존식은 항력(drag force), 양력(lift force), 다공성매체 저항력을 포함한다. 또한, 난류현상으로 standard k-${\varepsilon}$ 모델이 이용된다. 물과 기름 출구압은 oil separator 의 액위를 결정하는 중요한 인자이며, 정상운전상태 액위 25 cm를 맞추기 위하여 측정압은 각각 6.3 kPa, 5.1 kPa으로 결정되었다. 시간에 따른 공기, 물, 기름의 부피분율의 변화를 조사하였고, 정상상태에 도달하였을 때, 물과 기름상의 침강속도를 oil separator의 종축 길이에 따라 분석하였다. 본 연구에서 제시된 CFD 모델로부터 얻은 oil separator의 기름분리성능은 99.85%이며, 실험값과 거의 일치하였다. 비교적 단순한이 CFD 모델은향후 oil separator의구조를 변경하거나, 최적운전조건을 찾기위하여 유용하게사용될수있을 것이다.

Wind load on irregular plan shaped tall building - a case study

  • Chakraborty, Souvik;Dalui, Sujit Kumar;Ahuja, Ashok Kumar
    • Wind and Structures
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    • 제19권1호
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    • pp.59-73
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    • 2014
  • This paper presents the results of wind tunnel studies and numerical studies on a '+' plan shaped tall building. The experiment was carried out in an open circuit wind tunnel on a 1:300 scale rigid model. The mean wind pressure coefficients on all the surfaces were studied for wind incidence angle of $0^{\circ}$ and $45^{\circ}$. Certain faces were subjected to peculiar pressure distribution due to irregular formation of eddies caused by the separation of wind flow. Moreover, commercial CFD packages of ANSYS were used to demonstrate the flow pattern around the model and pressure distribution on various faces. k-${\varepsilon}$ and SST viscosity models were used for numerical study to simulate the wind flow. Although there are some differences on certain wall faces, the numerical result is having a good agreement with the experimental results for both wind incidence angle.

Numerical Simulation on the Performance of Axial Vane Type Gas-Liquid Separator with Different Guide Vane Structure

  • Yang, Fan;Liu, Ailan;Guo, Xueyan
    • International Journal of Fluid Machinery and Systems
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    • 제10권1호
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    • pp.86-98
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    • 2017
  • In order to obtain high efficiency and low resistance droplet separation apparatus, axial vane type gas-liquid separators with different guide vanes were designed, and the RNG $k-{\varepsilon}$ model as well as discrete phase model (DPM) were used to investigate the flow pattern inside the separators. It was shown that the tangential velocity distribution under different guide vanes have Rankine vortex characteristics, pressure distribution exhibits a high similarity which value becomes big as the increase of the blade outlet angle and the decrease of the guide vane numbers. The increase of the guide vane numbers and the decrease of the blade outlet angle could make separation improve significantly. The separation efficiency is almost 100% when the droplet diameter is bigger than $40{\mu}m$.

도로 터널내의 공기유동 양상을 예측하기 위한 수치해석 (Numerical Analysis to Predict Air Flow Phenomena in a Road Tunnel)

  • 최인수;박병덕;윤일로
    • 한국산업융합학회 논문집
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    • 제5권4호
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    • pp.313-320
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    • 2002
  • A 2-dimensional $k-{\varepsilon}$ numerical model was developed to explore the effects of vehicle movement, jet fan and wind speed for the ventilation of road tunnels. To consider the temperature distribution in the tunnel, the energy equation was solved with a source term of the energy exhausted from vehicles. Although the tunnel ventilation can be made by the piston effect of vehicle movement, an additional ventilation is necessary when a head wind is existing. Jet fans may assist the air flow in the tunnel. However, more efficient ventilation system should be necessary, because the exhaust gas from vehicles flow along the road surface and it cannot be diffused in the longitudinal tunnel.

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CFD 시뮬레이션을 이용한 농산물 저온저장고내의 온도분포 균일화 연구 (Uniformity of Temperature in Cold Storage Using CFD Simulation)

  • 정훈;권진경;윤홍선;이원옥;김영근;이현동
    • 한국식품저장유통학회지
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    • 제17권1호
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    • pp.16-22
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    • 2010
  • 농산물 저온저장고 내부의 온도분포 균일화를 수치해석적으로 분석하기 위해 3차원 CFD 시뮬레이션을 수행하였다. CFD 시뮬레이션 모델은 속도벡터 및 온도분포 측정치와 비교를 통해 검증하였으며, 온도분포 균일화 향상을 위한 적정 팬용량 및 적재방법을 설정하기 위해 몇 가지 팬풍속 및 저장물과 벽체간의 거리 등에 대해 기류패턴과 온도 분포를 분석하였다. CFD 시뮬레이션의 검증에서 속도벡터 분포는 PIV시스템에 의한 측정치와 비교했을 때 표준 k-$\varepsilon$모델 예측치와 측정치의 상대적 오차는 24.5%로 나타났고, RSM 모델 예측치와 측정치의 상대적 오차는 16.7%로 나타나 RSM 난류모델의 예측 정밀도가 더 높은 것으로 나타났다. 온도분포 검증 결과 실측치와 측정치의 R. M. S. 값은 농산물 무적재 상태에서 $0.33^{\circ}C$, 농산물 적재 상태에서는 $0.28^{\circ}C$로 나타났으며 예측값과 측정값의 온도분포 경향은 잘 일치하는 것으로 나타났다. 검증된 시뮬레이션 모델을 이용하여 $6{\times}10$열 2단 팔레트에 농산물이 적재되고 냉각용 송풍팬이 2개인 저온저장고에 대해 송풍팬의 풍량 및 저장물과 벽체와의 간격 변화의 영향을 분석한 결과, 저장물과 벽체와의 거리는 300 mm 이상, 송풍량은 300 CMM 이상에서 저장고 내의 공기 온도차는 $1^{\circ}C$이내로 유지되며 팔레트 사이에 간격을 둔 경우 온도분포의 균일성이 향상되는 것으로 나타났다.

기체구 분사 모델을 이용한 CNG 직접분사식 인젝터 분사 수치해석 기법 (Modeling of CNG Direct Injection using Gaseous Sphere Injection Model)

  • 최민기;박성욱
    • 한국분무공학회지
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    • 제21권1호
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    • pp.47-52
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    • 2016
  • This paper describes the modeling of CNG direct injection using gaseous sphere injection model. Simulation of CNG direct injection does not need break up and evaporation model compared to that of liquid fuel injection. And very fine mesh is needed near the injector nozzle to resolve the inflow boundary. Therefore it takes long computation time for gaseous fuel injection simulation. However, simulation of CNG direct injection could be performed with the coarse mesh using gaseous sphere injection model. This model was integrated in KIVA-3V code and RNG $k-{\varepsilon}$ turbulence model needs to be modified because this model tends to over-predict gas jet diffusion. Furthermore, we preformed experiments of gaseous fuel injection using PLIF (planar laser induced fluorescence)method. Gaseous fuel injection model was validated against experiment data. The simulation results agreed well with the experiment results. Therefore gaseous sphere injection model has the reliability about gaseous fuel direct injection. And this model was predicted well a general tendency of gaseous fuel injection.

Reliability of numerical computation of pedestrian-level wind environment around a row of tall buildings

  • Lam, K.M.;To, A.P.
    • Wind and Structures
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    • 제9권6호
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    • pp.473-492
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    • 2006
  • This paper presents numerical results of pedestrian-level wind environment around the base of a row of tall buildings by CFD. Four configurations of building arrangement are computed including a single square tall building. Computed results of pedestrian-level wind flow patterns and wind speeds are compared to previous wind tunnel measurement data to enable an assessment of CFD predictions. The CFD model uses the finite-volume method with RNG $k-{\varepsilon}$ model for turbulence closure. It is found that the numerical results can reproduce key features of pedestrian-level wind environment such as corner streams around corners of upwind building, sheltered zones behind buildings and channeled high-speed flow through a building gap. However, there are some differences between CFD results and wind tunnel data in the wind speed distribution and locations of highest wind speeds inside the corner streams. In locations of high ground-level wind speeds, CFD values match wind tunnel data within ${\pm}10%$.

Numerical Study on Flow Characteristics at Blade Passage and Tip Clearance in a Linear Cascade of High Performance Turbine Blade

  • Myong, Hyon-Kook;Yang, Seung-Yong
    • Journal of Mechanical Science and Technology
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    • 제17권4호
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    • pp.606-616
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    • 2003
  • A numerical analysis has been conducted in order to simulate the characteristics of complex flow through linear cascades of high performance turbine blade with/without tip clearance by using a pressure-correction based, generalized 3D incompressible Wavier-Stokes CFD code. The development and generation of horseshoe vortex, passage vortex, leakage vortex, tip vortex within tip clearance, etc. are clearly identified through the present simulation which uses the RNG k-$\varepsilon$ turbulent model with wall function method and a second-order linear upwind scheme for convective terms. The present simulation results are consistent with the generally known tendency that occurs in the blade passage and tip clearance. A 3D model for secondary and leakage flows through turbine cascades with/without tip clearance is also suggested from the present simulation results, including the effects of tip clearance height.

Numerical Prediction of Turbulent Flow in Bare Rod Bundles Using Control Volume Based Finite Element Method

  • Im, In-Young;Cheong, Jong-Sik
    • 한국원자력학회:학술대회논문집
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    • 한국원자력학회 1995년도 추계학술발표회논문집(1)
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    • pp.480-486
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    • 1995
  • Turbulent flow field in a subchannel of bare rod bundles has been numerically simulated using the control volume based finite element method. Launder & Ying model of Reynolds stress and Lam & Bremhorst low-Reynolds number model are implemented in k-$\varepsilon$ equations and momentum equations. Secondary flows are simulated using the stream function and vorticity approach. The control volume based finite element method enable to use the upwind scheme (donor cell scheme). Sensitivity of the constants in the models are studied, and proper values are found to get the close result to the measured flow distributions.

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