• 제목/요약/키워드: Logarithmic turbulent equation

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유한요소법을 이용한 난류유동해석 (The Turbulent flow analysis by the Finite Element Method)

  • 황상무
    • 한국소성가공학회:학술대회논문집
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    • 한국소성가공학회 1999년도 춘계학술대회논문집
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    • pp.253-256
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    • 1999
  • The Streamline Upwind Petrov-Galerkin(SUPG) finite element method is used to solve the two-dimensional laminar and turbulent flow. The flow is simulated by averaged Navier-Stokes equations with a penalty function approach and the lograithmic(k-$\varepsilon$) turbulent model is employed to take into account its turbulent behavior. The near-wall viscous sub-layer model is employed to approach the dominant viscous effects in the near wall zones. To find a good-enough initial guess of the Newton-Raphson iteration solving Nonlinear Matrix the Incremental method is considered for momentum and the Incomplete logarithmic turbu-lent equations for Turbulence. The validation of our method is investigated in comparision with published experimental data.

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난류전단 흐름에서의 기포응집에 관한 수치모의: 1. 모형의 개발 (Numerical Simulation of the Coalescence of Air Bubbles in Turbulent Shear Flow: 1. Model Development)

  • 전경수
    • 대한토목학회논문집
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    • 제14권6호
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    • pp.1357-1363
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    • 1994
  • 난류전단 흐름에서의 기포응집에 따른 기포의 크기분포를 예측하기 위한 Monte-Carlo 모의모형을 개발하였다. 임의로 선택된 각 초기위치에 일련의 기포들을 매시각 발생시키고, 각 기포들의 움직임과 충돌을 모의함으로써 각각의 위치와 크기를 추적하도록 하였다. 기포의 횡방향 변위는 이송확산 방정식의 수치해를 이용하여 부여하였으며, 종방향 변위는 흐름의 대수유속분포 및 기포 상승속도로부터 주어지도록 하였다. 각 기포들간의 초기 상대위치와 상대변위를 이용한 기하학적 해석에 의하여 매시간단계에서의 기포응집을 탐지하여, 시간단계 말기에서의 기포 총수, 각 기포의 위치 및 크기를 결정하였다. 기포들의 크기 및 위치를 나타내기 위하여 소요되는 기억용량을 최소화하도록 전산모형을 구성하였다.

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고 레이놀즈수 유동의 수치해석시 벽함수 사용에 관한 연구 (A Study of using Wall Function for Numerical Analysis of High Reynolds Number Turbulent Flow)

  • 최정규;김형태
    • 대한조선학회논문집
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    • 제47권5호
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    • pp.647-655
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    • 2010
  • In this paper, a numerical study is carried out for super-pipe, flat plate and axisymmetric body flows to investigate a validity of using wall function and high $y_1^+$ in calculation of high Reynolds number flow. The velocity profiles in boundary layer agree well with the law of the wall. And it is found that the range of $y^+$��which validated the logarithmic law of the wall grows with increasing Reynolds number. From the result, an equation is suggested that can be used to estimate a maximum $y^+$ value of validity of the log law. And the slope(1/$\kappa$) of the log region of the numerical result is larger than that of experimental data. On the other hand, as $y_1^+$ is increasing, both the friction and the pressure resistances tend to increase finely. When using $y_1^+$ value beyond the range of log law, the surface shear stress shows a significant error and the pressure resistance increases rapidly. However, when using $y_1^+$ value in the range, the computational result is reasonable. From this study, the use of the wall function with high value of $y_1^+$ can be justified for a full scale Reynolds number ship flow.