• 제목/요약/키워드: k-epsilon turbulence model

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수력학적 공동현상을 이용한 온수 발생 장치에서의 회전체 형상에 대한 수치해석적 연구 (A Numerical Simulation Study on the Shape of the Rotor in Hydraulic Cavitation Heat Generator)

  • 손손;신명섭;이웅엽;엄애선;윤준용
    • 한국유체기계학회 논문집
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    • 제20권2호
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    • pp.75-81
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    • 2017
  • This paper presents a numerical investigation on the local hydraulic cavitation phenomena of water resulting from the rotor with high rotational speed in the hydraulic cavitation heat generator. The numerical simulation utilizes the standard k-epsilon turbulence model, the mixture multiphase model and the Schnerr-Sauer cavitation model to simulate the complex cavitation phenomena in the generator. For exploring the efficient shape of the dimples on the rotor to causing cavitation phenomena artificially, the pressure distributions and the volume fractions of the vapor on the rotor are investigated respectively about different shapes of the rotor in the generator. The optimum shape of the dimple to causing cavitation phenomena in the selected shapes is obtained by the means of the numerical simulation.

공탄성 변형효과를 고려한 5MW급 풍력발전 블레이드의 피치각에 따른 성능해석 (Aerodynamic and Structural Design of 6kW Class Vertical-Axis Wind Turbine)

  • 김요한;김동현;황미현;김경희;황병선;홍은성
    • 한국유체기계학회 논문집
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    • 제14권3호
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    • pp.39-44
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    • 2011
  • In this study, performance analyses have been conducted for a 5MW class wind turbine blade model. Advanced computational analysis system based on computational fluid dynamics(CFD) and computational structural dynamics(CSD) has been developed in order to investigate detailed dynamic responsed of wind turbine blade. Reynolds-averaged Navier-Stokes (RANS) equations with K-${\epsilon}$ turbulence model are solved for unsteady flow problems of the rotating turbine blade model. A fully implicit time marching scheme based on the Newmark direct integration method is used for computing the coupled aeroelastic governing equations of the 3D turbine blade for fluid-structure interaction (FSI) problems. Predicted aerodynamic performance considering structural deformation effect of the blade show different results compared to the case of rigid blade model.

액체분무의 증발 및 연소에 관한 수치적 연구 (A Numerical Study on Evaporation and Combustion of Liquid Spray)

  • 정인철;이상용;백승욱
    • 대한기계학회논문집
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    • 제15권6호
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    • pp.2073-2082
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    • 1991
  • 본 연구에서는 선회유동과 재순환영역이 있는 제한된 동축 분류유동(confined coaxial jet flow)을 갖는 연소기에 대하여 노즐을 통하여 분사된 연료액적의 증발 및 연소, 그리고 주위기체유동에 관한 제반현상을 정상상태 하에서 모사하고자 하는데 그 목적이 있으며 수치계산에 의한 이론적 해석방법으로 기상은 오일러 방식, 액상은 라 그란지 방식을 채택하였고 후술될 증발 및 연소모델을 적용하였다.

교차된 관군에 수직한 난류유동 및 난류열전달의 수치해석 (Numerical Analysis of Turbulent Flow and Heat Transfer Normal to a Staggered Tube Bank)

  • 이건휘;이병곤;최영돈
    • 대한기계학회논문집
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    • 제15권1호
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    • pp.218-228
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    • 1991
  • Since heat exchangers are composed of bank of tubes, the knowledge on the flow and heat transfer characteristics of the tube bank are required for the optimum design and selection of heat exchangers. In this paper, the turbulent flow fields and heat transfers normal to a staggered tube bank are solved numerically employing K-.epsilon. 2 equation turbulence model and non-orthogonal coordinate transformation for the treatment of curved surface of tubes. Predicted mean Nusselt numbers of tube bank agree reasonably well with Grimision's correlation

형상 최적화를 통한 축류송풍기의 설계 (Design of An Axial Flow Fan with Shape Optimization)

  • 서성진;최승만;김광용
    • 대한기계학회논문집B
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    • 제30권7호
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    • pp.603-611
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    • 2006
  • This paper presents the response surface optimization method using three-dimensional Wavier-Stokes analysis to optimize the blade shape of an axial flow fan. Reynolds-averaged Wavier-Stokes equations with $k-{\epsilon}$ turbulence model are discretized with finite volume approximations using the unstructured grid. Regression analysis is used for generating response surface, and it is validated by ANOVA and t-statistics. Four geometric variables, i.e., sweep and lean angles at mean and tip respectively were employed to improve the efficiency. The computational results are compared with experimental data and the comparisons show generally good agreements. As a main result of the optimization, the total efficiency was successfully improved. Also, detailed effects of sweep and lean on the axial flow fan are discussed.

엔진룸 내의 열유체 유동의 2차원 수치시뮬레이션 (A two-dimensional numerical simulation of the thermal and fluid flow in engine room)

  • 유정열;윤홍열;이훈구
    • 오토저널
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    • 제14권6호
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    • pp.99-104
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    • 1992
  • The complex geometry of the engine room of a passenger car has been modelled two-dimensionally and the thermal and fluid flow therein have been analyzed by using a commercially available code, PATRAN/FLORAM$\mid$N. FLOTRAN adopts a finite element method with streamline upwind formulation for convective terms and the k-.epsilon. turbulence model to solve the three dimensional turbulent flow and heat transfer problems. Velocity vectors, pressure and temperature distributions have been obtained for various cases with different arrangements of license plate, underbody-covers and air dams. The results show that the numerical analysis using PATRAN/FLOTRAN can predict qualitatively well the practical phenomena.

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핵연료 집합체 혼합날개형상의 수치최적설계 (Numerical Optimization of the Shape of Mixing Vane in Nuclear Fuel Assembly)

  • 서준우;김광용
    • 대한기계학회논문집B
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    • 제28권8호
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    • pp.929-936
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    • 2004
  • In the present work, shape of the mixing vane in Plus7 fuel assembly has been optimized numerically using three-dimensional Reynolds-averaged Navier-Stokes analysis of flow and heat transfer. Standard $k-{\epsilon}$ model is used as a turbulence closure. The Response surface method is employed as an optimization technique. The objective function is defined as a combination of heat transfer rate and inverse of friction loss. Bend angle and base length of mixing vane are selected as design variables. Thermal-hydraulic performances for different shapes of mixing vane have been discussed, and optimum shape has been obtained as a function of weighting factor in the objective function.

제트송풍기 노즐의 형상최적설계 (Design Optimization of Nozzle Shape for a Jet Fan)

  • 서성진;김광용
    • 대한기계학회논문집B
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    • 제30권8호
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    • pp.715-721
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    • 2006
  • In the present work, nozzle shape of a jet fan is optimized numerically using three-dimensional Reynolds-averaged Navier-Stokes analysis. Standard $k-{\epsilon}$ model is used as a turbulence closure. Response surface method is employed as an optimization technique. The objective function is defined as maximum throw distance. Three geometric variables, i.e., length and angle of nozzle, and interval between two nozzles, are selected as design variables. As the main result of the optimization, the throw distance has been improved effectively.

비균일 단면을 가진 철도차량의 내부 열유동 해석 (Numerical Analysis on HVAC Characteristics of Train with non-uniform Interior Cross-section)

  • 남성원;김형진
    • 한국철도학회:학술대회논문집
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    • 한국철도학회 2004년도 춘계학술대회 논문집
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    • pp.685-689
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    • 2004
  • Numerical simulation is conducted to clarify the heat transfer and fluid flow characteristics of HVAC(Heating, Ventilating and Air-Conditioning) for double' deck train. The HVAC system is installed under the roof of carbody. In the lay-out of HVAC system, air duct must be installed to supply air to 1st and 2nd floor respectively. The standard k-$\epsilon$ and LES models for turbulence and SIMPLE algorithm for pressure equation hased on finite volume method are used to solve the physic a] HVAC model. To assure convergence, QUICK scheme for momentum equation and the 2nd order upwind scheme for turbulent equations arc used. From the results of simulation, the temperature and velocity magnitude are also distributed uniformly in the interior of double-deck passenger car.

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압력 평형식 온도 조절 밸브의 유동특성 연구 (A study on the flow charateristics of temperature control valve by pressure compensation)

  • 김태안;김윤제
    • 유체기계공업학회:학술대회논문집
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    • 유체기계공업학회 2001년도 유체기계 연구개발 발표회 논문집
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    • pp.419-424
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    • 2001
  • TCV(Temperature control valve by pressure compensation) controls temperature constantly, when it is sending steam or high temperature water to heating device of heat exchanger. For designing TCV, the ratio of piston and hole diameters is one of the important design parameters. Numerical analysis is carried out to elucidate the flow characteristics in the TCV with different port areas of cold and hot waters, using the k-$\epsilon$ turbulence model and Cartesian cut-cell method. Numerical results show that the exit flow rate is mainly affected by pressure distribution in the piston.

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