• 설비공학논문집
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• 제15권10호
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• pp.809-820
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• 2003

The present study investigates effects of flow velocity on the convective heat/mass transfer characteristics in wavy ducts of a primary surface heat exchanger application. Local heat/mass transfer coefficients on the wavy duct sidewall are determined by using a naphthalene sublimation technique. The flow visualization technique is used to understand the overall flow structures inside the duct. The aspect ratio and corrugation angle of the wavy duct is fixed at 7.3 and 145$^{\circ}$ respectively, and the Reynolds numbers, based on the duct hydraulic diameter, vary from 100 to 5,000. The results show that there exist complex secondary flows and transfer processes resulting in non-uniform distributions of the heat/mass transfer coefficients on the duct side walls. At low Re (Re<1000), relatively high heat/mass transfer regions like cell shape appear on both pressure and suction side wall due to the secondary vortex flows called Taylor-Gortler vortices perpendicular to the main flow direction. However, at high Re (Re>1000), these secondary flow cells disappear and boundary layer type flow characteristics are observed on pressure side wall and high heat/mass transfer region by the flow reattachment appears on the suction side wall. The average heat/mass transfer coefficients are higher than those of the smooth circular duct due to the secondary flows inside wavy duct. And also friction factors are about two times greater than those of the smooth circular duct.

• 대한기계학회논문집B
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• 제30권6호
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• pp.578-586
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• 2006

Numerical simulations are carried out to investigate the thermal effects of the gravitational potential on the centrifugal instability of a Taylor-Couette flow, and to further study the detailed flow fields and flow bifurcations to spiral vortices. The effects of centrifugal potential on the centrifugal instability are also investigated in the current study. Spiral vortices have various types of mode depending on Grashof number and Reynolds number. The correlation of Richardson number with the spiral angle of the spiral vortices shows that the structure of the spiral vortices strongly depends on the Richardson number. The heat transfer rate of the inner cylinder increases with increasing Grashof number. It is also confirmed that the torque required to rotate the inner cylinder increases as Grashof number increases.

• Journal of Advanced Marine Engineering and Technology
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• 제27권3호
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• pp.460-465
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• 2003

Microgravity experiments were conducted to determine the effect of liquid and gas superficial velocities on flow behaviors. Flow behaviors observed under microgravity conditions can be classified into five flow patterns: bubble. Taylor bubble, slug, semi-annular and annular flows. Transition boundary between four flow patterns could be determined by drift-flux model. It was also found that the effect of gravity and pipe inclination on flow pattern transition was not significant in the inertia dominant region.

• 한국콘텐츠학회논문지
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• 제11권1호
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• pp.404-410
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• 2011

1차원 개수로 부정류의 수치 해석을 위하여 Taylor-Galerkin 기법의 유한요소법을 St. Venant 방정식의 차분에 적용하였다. 단일 수로에서 수문의 닫힘에 의한 배수문제와 3개 이상 하도가 만나는 합류점을 포함하는 수지상(dendritic) 하천 네트워크에 적용하고 그 결과를 기존에 제시된 유한차분법, 유한요소법 등의 수치기법과 비교하였으며 매우 잘 일치함을 확인하였다. 본 연구에서 적용한 기법은 연속방정식과 운동량방정식을 순차적으로 해석해 나가기 때문에 적용이 간편하며, 최종적으로 삼대각 행렬과 합류점의 적합조건을 위한 최소한의 요소를 포함하기 때문에 삼대각 행렬의 연산 방법을 적용할 수 있어 계산 측면에서 빠르고 안정적이다. 또한, 행렬의 저장을 위한 메모리 측면에서 경제적이다.

• 한국수자원학회논문집
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• 제37권2호
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• pp.87-96
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• 2004

Li 등(1998)이 제안한 호안제체를 통과하는 non-Darcy 흐름에 대한 i- V관계식의 해석결과는 실측자료와의 비교결과 잘 맞는 것으로 나타났다. 따라서 이식의 사용은 현장에 적용성이 있는 것으로 평가되었고, 적용에 따른 변수인 공극율의 정확한 값의 입력이 요구된다. 관수로흐름과 Taylor의 평균수리수심에 기초한 사석에 적용되는 non-Darcy 특성의 흐름은 블록 및 케이슨 호안에도 적용 가능한 것으로 평가된다. 호안제체를 통과하는 흐름에 대한 정확한 계산은 호안의 최종체절 개방구간에서의 정확한 유속의 산정은 물론 축조 후의 호안 내의 수위의 변화를 예측할 수 있다.

• 한국전산유체공학회지
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• 제1권1호
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• pp.88-97
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• 1996

This paper treats an adaptive finite-element method for the viscous compressible flow governed by Navier-Stokes equations in two dimensions. The numerical algorithm is the two-step Taylor-Galerkin mettled using unstructured triangular grids. To increase accuracy and stability, combined moving node method and grid refinement method have been used for grid adaption. Validation of the present algorithm has been made by comparing the present computational results with the existing experimental data and other numerical solutions. Four benchmark problems are solved for demonstration of the present numerical approach. They include a subsonic flow over a flat plate, the Carter flat plate problem, a laminar shock-boundary layer interaction. and finally a laminar flow around NACA0012 airfoil at zero angle of attack and free stream Mach number of 0.85. The results indicates that the present adaptive triangular grid method is accurate and useful for laminar viscous flow calculations.

• 대한기계학회논문집
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• 제19권3호
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• pp.834-845
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• 1995

An experimental study is made in a nearly two-dimensional 90.deg. curved duct to investigate the effects of interaction between streamline curvature and mean strain on turbulence. The initial shear at the entrance to the curved duct is varied by an upstream shear generator to produce five different shear conditions ; a uniform flow (UF), a positive weak shear (PW), a positive strong shear(PS), a negative weak shear (NW) and a negative strong shear(NS). With the mean field data of the case UF, variations of the momentum thickness, the shape factor and the skin friction over the convex(inner) surface and the concave (outer) surface are scrutinized quantitatively in-depth. It is found that, while the pressure loss due to curvature is insensitive to the inlet shear rates, the distributions of wall static pressure along both convex and concave surfaces are much influenced by the inlet shear rates.

• 대한기계학회논문집B
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• 제33권6호
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• pp.443-453
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• 2009

The Rayleigh-Taylor instability, the bubble rising in both partially and fully filled containers and the droplet splash are simulated by an in-house solution code(PowerCFD), which are typical benchmark problems among multiphase flows with material interface due to density difference. The present method(code) employs an unstructured cell-centered method based on a conservative pressure-based finite-volume method with interface capturing method(CICSAM) in a volume of fluid(VOF) scheme for phase interface capturing. The present results are compared with other numerical solutions found in the literature. It is found that the present method simulates efficiently and accurately complex free surface flows such as multiphase flows with material interface due to both density difference and instability.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2008년도 춘계학술대회논문집
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• pp.572-575
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• 2008

Two-dimensional multiphase flows due to density difference such as the Rayleigh-Taylor instability problem and the droplet splash are simulated by an in-house solution code(PowerCFD). This code employs an unstructured cell-centered method based on a conservative pressure-based finite-volume method with interface capturing method in a volume of fluid(VOF) scheme for phase interface capturing. The present results are compared with other numerical solutions found in the literature. It is found that the present code simulates complex free surface flows such as multiphase flows due to density difference efficiently and accurately.

• 한국추진공학회지
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• 제17권6호
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• pp.81-88
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• 2013

Taylor-Maccoll 유동관계식과 준 1차원 모델을 적용한 구성품 기반의 이중램제트 추진기관 모델 개발에 대해 기술하였다. 이중램제트 흡입구는 Taylor Maccoll 유동관계식을 적용하여 콘 각도 $25^{\circ}$ 형상을 갖는 흡입구에 대해 아음속 및 초음속 흡입구 모델을 구현하였으며 예 연소가스를 초음속 연소기로 전달하는 기능의 가스발생기는 Lumped 모델을 적용하여 모델을 구현하였고 요구되는 노즐목 크기에 대해 기술하였다. 초음속 연소기의 경우 준 1차원 모델을 적용하여 위치에 따른 마하수 변화, 온도변화 및 압력변화 등을 제시하였다. 또한 금번 모델을 이용하여 당량비 및 압력회복율을 고려한 연료량 조절모델에 따른 추력과 비추력을 계산하여 그 결과를 제시하였다.