• 제목/요약/키워드: k-$\varepsilon$ turbulence model

검색결과 467건 처리시간 0.025초

사류송풍기의 유동해석 및 최적설계 (Flow analysis and design optimization of a mixed-flow fan)

  • 서성진;전재욱;김광용
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2001년도 춘계학술대회논문집E
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    • pp.684-689
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    • 2001
  • In this study, three-dimensional viscous flow analysis and optimization are presented for the design of a mixed-flow fan. Steady, imcompressible, three-dimensional Reynolds averaged Navier-Stokes equations are used as governing equations, and standard $k-{\varepsilon}$ turbulence model is chosen as a turbulence model. Governimg equations are discretized using finite volume method. Upwind difference scheme is used for the discretization of the convective term and SIMPLEC algorithm is used as a velocity-pressure correction procedure. The computational results are compared with the results obtained by TASCflow. For the numerical optimization of the design, objective function is defined as a ratio of generation of the turbulent energy to pressure head. Sweep angles are used as design variables.

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축류송풍기의 저소음 설계에서 수치최적화기법들의 평가 (Assessment of Numerical Optimization Algorithms in Design of Low-Noise Axial-Flow Fan)

  • 최재호;김광용
    • 대한기계학회논문집B
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    • 제24권10호
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    • pp.1335-1342
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    • 2000
  • Three-dimensional flow analysis and numerical optimization methods are presented for the design of an axial-flow fan. Steady, incompressible, three-dimensional Reynolds-averaged Navier-Stokes equations are used as governing equations, and standard k- ${\varepsilon}$ turbulence model is chosen as a turbulence model. Governing equations are discretized using finite volume method. Steepest descent method, conjugate gradient method and BFGS method are compared to determine the searching directions. Golden section method and quadratic fit-sectioning method are tested for one dimensional search. Objective function is defined as a ratio of generation rate of the turbulent kinetic energy to pressure head. Two variables concerning sweep angle distribution are selected as the design variables. Performance of the final fan designed by the optimization was tested experimentally.

반응면 기법을 이용한 제트송풍기의 공력학적 수치최적설계 (Aerodynamic Design Optimization of an Jet Fan using the Response Sruface Method)

  • 서성진;김광용
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2002년도 학술대회지
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    • pp.635-638
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    • 2002
  • In this study, three-dimensional imcompressible viscous flow analysis and optimization using response surface method are presented for the design of a jet fan. Steady, imcompressible, three-dimensional Reynolds averaged Wavier-Stokes equations are used as governing equations, and standard $k-{\varepsilon}$ turbulence model is chosen as a turbulence model. Governimg equations are discretized using finite volume method. Sweep angles are used as design variables for the shape optimization of the impeller in response surface method. The experimental points which are needed to construct response surface are obtained from the D-optimal design and finally the shape of impeller Is achieved from using a numerical optimization for the response surface which is obtained from CFD.

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원자로 부수로내 혼합날개를 지나는 삼차원 열유동 해석 (Numerical Analyses of Three-Dimensional Thermo-fluid flow through Mixing Vane in A Subchannel of Nuclear Reactor)

  • 최상철;김광용
    • 대한기계학회논문집B
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    • 제27권3호
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    • pp.311-318
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    • 2003
  • The present work evaluates the effects of mixing vane shape on the flow structure and heat transfer downstream of mixing vane in a subchannel of fuel assembly. by obtaining velocity and pressure fields. turbulent intensity. flow-mixing factors. heat transfer coefficient and friction factor using three-dimensional RANS analysis. Four different shapes of mixing vane. which were designed by the authors were tested to evaluate the performances in enhancing the heat transfer. Standard k-$\varepsilon$ model is used as a turbulence closure model. and. periodic and symmetry conditions are set as boundary conditions. The flow blockage ratio is kept constant. but the twist angle of mixing vane is changed. The results with three turbulence models were compared with experimental data.

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.

원추형 디퓨져 내의 난류운동에 관한 수치해석적 연구 (Numerical Study on Turbulent Flow in a Conical Diffuser)

  • 강신형;최영석
    • 대한기계학회논문집
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    • 제16권10호
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    • pp.1971-1978
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    • 1992
  • 본 연구에서는 원형 파이프에 원추형 디퓨져가 연결된 덕트 내의 유동장에 대 하여 Launder-Sharma의 저 레이놀즈수 k-.epsilon. 난류모델을 이용하여 수치해석을 수행하였 으며, 수치해석 방법으로는 타원형 방법을 사용하였으며, 앞으로 일반적인 단면의 곡 관이나 스크롤 내부 유동 등의 연구 수행을 감안하여 지배방정식을 일반 비직교 좌표 계로 변환하여 계산을 수행하였다.

A numerical study of the turbulent fluctuating flow around a square cylinder for different inlet shear

  • Islam, A.K.M. Sadrul;Hasan, R.G.M.
    • Wind and Structures
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    • 제5권1호
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    • pp.15-24
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    • 2002
  • This paper reports the numerical calculations of uniform turbulent shear flow around a square cylinder. The predictions are obtained by solving the two-dimensional unsteady Navier-Stokes equations in a finite volume technique. The turbulent fluctuations are simulated by the standard $k-{\varepsilon}$ model and one of its variant which takes care of the realizability constraint in order to suppress the excessive generation of turbulence in a stagnation condition. It has been found that the Strouhal number and the mean drag coefficient are almost unaffected by the shear parameter but the mean lift coefficient is increased. The present predictions are compared with available experimental data.

가압중수형 원자로의 중성자 감속재 순환 유동가시화와 삼차원 전산해석 (Visualization and 3D Numerical Analysis of the Circulation Flow of the Neutron Moderator in a Heavy-Water Nuclear Reactor)

  • 엄태광;이재영
    • 대한기계학회논문집B
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    • 제36권2호
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    • pp.189-196
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    • 2012
  • 현 운행중인 중수로의 안전장치인 감속재는 원전사고시 최종 열침원의 역할을 감당한다. 감속재 연구 수행을 위해 CANDU6 의 축소화 모델인 HUKINS 는 최대출력 10kW 로, 칼란드리아 직경은 원모델의 1/8 에 해당하는 0.95m 이며 축방향 길이가 38.4mm 의 열원 88 개가 삽입되어 있다. HUKINS 내 감속재 유동패턴의 발생 여부를 판단하고자 화학처리기법을 활용하였고 그 결과 출력파워 약 7.7kW 에서 각입력유량을 4,7,11L/min 으로 유입시 감속재의 유동패턴이 부력기조유동, 혼합양상유동, 모멘텀 기조유동의 양상을 나타났다. 3 가지 유동패턴에 대해 육면체 격자를 기본으로 구성된 약 190 만개의 격자수 내에서 난류모델 $k{\varepsilon}$의 예측결과와 실험결과간에 유사성을 보임으로써 HUKINS 가 CANDU6 감속재 유동의 실험적 연구에 사용 가능함을 입증했다.

쇄파대에서 정현파의 쇄파 (Wave Breaking of Sinusoidal Waves in the Surf Zone)

  • 황종길;김영택;조용식
    • 한국수자원학회논문집
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    • 제37권6호
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    • pp.461-466
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    • 2004
  • 본 연구에서는 쇄파대에서 정현파의 쇄파에 대해 수리모형실험과 수치모형실험을 수행하였으며, 두 실험결과를 비교하였다. 수치해석 모형에서는 Reynolds 방정식을 지배방정식으로 사용하고 난류해석을 위해 $textsc{k}$-$\varepsilon$ 모델을 적용하였으며, 자유수면변위를 추적하기 위해 VOF기법을 사용하였다. 수리모형실험과 수치모형실험 모두 동일한 수심과 주기를 가질 경우, 입사파의 파고가 커질수록 쇄파발생 지점이 경사시작 지점으로부터 가까운 위치로 이동하는 경향을 보였다. 또한, 쇄파발생시 파고비(H/H$_{0}$)는 동일한 수심과 파고를 가질 경우, 주기가 커질수록 증가하는 경향을 보였다.

수조 수치실험에 의한 말뚝구조물의 항력계수 산정 (Drag Coefficient Estimation of Pile Type Structures by Numerical Water Basin Experiments)

  • 박일흠;이근효;조영준
    • 한국해안·해양공학회논문집
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    • 제21권1호
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    • pp.45-53
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    • 2009
  • RNG $k-{\varepsilon}$ 난류모형이 포함된 3차원 동수역학 수치모형(FLOW-$3D^{(R)}$)을 사용하여 수조 수치실험을 통한 항력계수 산정 가능성을 검토하였다. 물리적 실험으로 항력계수가 알려져 있는 말뚝구조물에 대하여, 사각형 말뚝구조물의 수치해에 의한 항력계수값이 $1.34{\sim}1.52$로 물리적 실험값인 $1.3{\sim}1.5$의 범위와 매우 유사한 결과를 보였다. 원형 말뚝구조물은 0.5$0.75{\sim}0.78$ 정도로서 물리적 실험치와 비교적 잘 일치하였다. 그리고 항력계수값이 알려지지 않은 열을 이룬 말뚝구조물의 경우 항력계수값은 구조물 간의 간섭으로 단일 구조물에 비해 항력계수가 크게 나타났으며, 각 구조물간의 거리비가 작아짐에 따라 구조물이 받는 항력계수값은 증가하는 양상을 보였다.