• 태양에너지
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• 제14권2호
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• pp.51-60
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• 1994

본 연구에서는 Furan foundry sand 유동층에서 유동화 특성과 Single spiral coil tube에 대한 열전달 특성을 실험하였으며, 전열관의 Pitch와 직경의 비(p/Do=1.58, 2.37, 3.17, 4.75) 및 전열관의 Pitch와 유동입자 크기의 비(p/dp=21.25, 25.15, 30.18, 35.93)가 전열특성에 미치는 영향을 실험적으로 연구하였다. 그 결과 다음과 같은 결론을 얻었다. 1) p/Do가 증가 할수록 평균 열전달계수는 증가한다. 2) 평균 Nusselt수의 증가율은 p/Do=4.75일 때보다 1.58 일 때가 더 크다. 3) 평균 Nusselt수와 Re수, $Pr_g$수 및 p/dp의 상관 관계식은 다음과 같이 나타낼 수 있었다. $Nu_{mean}=C\;Re^m\;Pr_g^{0.4}(p/dp)^n$.

• 태양에너지
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• 제15권3호
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• pp.105-117
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• 1995

본 연구소에서는 Furan foundry sand 유동층내에 Spiral coil tube를 설치하여 유동입자, 유동층내 온도, 유동율, 전열 관의 Pitch와 직경 비(p/Do) 및 전열 관의 Pitch와 유동입자의 크기의 비(p/dp) 등이 전열 관 표면 열 전달계수(ho)에 미치는 영향을 실험적으로 연구하고, 또한 최대 $Nu_{max}$수를 여러 변수들의 관계로 나타내었다. 전열 관 표면 열 전달계수는 유동층내 온도가 높아 질 수록, 유동율이 커질수록 증가한다. 그러나 유동입자의 크기가 커지면 열 전달계수는 감소한다. 전열 관의 Pitch와 직경 비(p/Do)와의 관계에서 p/Do=4.75일 때 가장 높은 열 전달계수를 얻었으며, 유동층내 온도가 상승하고, Re 수가 증가할 수록 p/Do=1.58일 때보다 p/Do=4.75일때가 Nu수의 증가율은 다소 감소하는 경향을 보였다. 또한 p/dp의 비가 클 경우 낮은 온도($75^{\circ}C$)에서, p/dp의 비가 작을 경우는 높은 온도($550^{\circ}C$)에서 열 전달 효과가 큰 것으로 나타났다. 본 실험범위에서 최대 $Nu_{max}$ 수와 Re 수, Prg 수, p/dp 및 p/Do의 관계를 무차원 식으로 다음과 같이 나타낼 수 있었다. $$Nu_{max}=1.01\;Re^{0.48}Prg^{0.4}(p/dp)^{0.28}(p/Do)^{0.05}$$.

• 대한기계학회논문집B
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• 제30권7호
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• pp.700-706
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• 2006

This study presents a numerical procedure to optimize the shape of dimple surface to enhance turbulent heat transfer in a rectangular channel. The response surface based optimization method is used as an optimization technique with Reynolds-averaged Wavier-Stokes analysis of fluid flow and heat transfer with shear stress transport (SST) turbulence model. The dimple depth-to-dimple print diameter ratio, channel height-to-dimple print diameter ratio, and dimple print diameter-to-pitch ratio are chosen as design variables. The objective function is defined as a linear combination of heat transfer related term and friction loss related term with a weighting factor. full factorial method is used to determine the training points as a mean of design of experiment. The optimum shape shows remarkable performance in comparison with a reference shape.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2007년도 춘계 학술대회논문집
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• pp.159-162
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• 2007

This study presents a numerical procedure to optimize the shape of a staggered dimpled surface to enhance the turbulent heat transfer in a rectangular channel. A optimization technique based on neural network is used with Reynolds-averaged Navier-Stakes analysis of the fluid flow and heat transfer with Shear Stress Transport turbulence model. The dimple depth-to-dimple print diameter ratio, channel height-to-dimple print diameter ratio, and dimple print diameter-to-pitch ratio are chosen as design variables. The objective function is defined as a linear combination of terms related to heat transfer and friction loss with a weighting factor. Latin Hypercube Sampling is used to determine the training points as a mean of the Design of Experiment. Optimal values of the design variables were obtained in a range of the weighting factor.

• 유체기계공업학회:학술대회논문집
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• 유체기계공업학회 2004년도 유체기계 연구개발 발표회 논문집
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• pp.285-288
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• 2004

This study presents a numerical procedure to optimize the shape of dimple surface to enhance turbulent heat transfer in rectangular channel. The response surface based optimization method is used as an optimization technique with Reynolds-averaged Wavier-Stokes analysis of fluid flow and heat transfer with shear stress transport (SST) turbulence model. The dimple depth-to -dimple print diameter ratio, channel height- to- dimple print diameter ratio. and dimple print diameter-to-pitch ratio are chosen as design variables. The objective function is defined as a linear combination of heat transfer coefficient and friction drag coefficient with a weighting factor. Full factorial method is used to determine the training points as a mean of design of experiment.

• 한국유체기계학회 논문집
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• 제10권3호
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• pp.39-46
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• 2007

This study presents a numerical procedure to optimize the shape of staggered dimple surface to enhance turbulent heat transfer in a rectangular channel. The RBNN method is used as an optimization technique with Reynolds-averaged Navier-Stokes analysis of fluid flow and heat transfer with shear stress transport (SST) turbulence model. The dimple depth-to-dimple print diameter (d/D), channel height-to-dimple print diameter ratio (H/D), and dimple print diameter-to-pitch ratio (D/S) are chosen as design variables. The objective function is defined as a linear combination of heat transfer related term and friction loss related term with a weighting factor. Latin Hypercube Sampling (LHS) is used to determine the training points as a mean of the design of experiment. The optimum shape shows remarkable performance in comparison with a reference shape.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2003년도 추계학술대회
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• pp.598-603
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• 2003

A CFD analysis has been performed to investigate turbulent heat transfer in a triangular rod bundle with a pitch-to-diameter ratio(P/D) of 1.06. Anisotropic turbulence models predicted the turbulence-driven secondary flow in the triangular subchannel and the distributions of time mean velocity and temperature showing significantly improved agreement with the measurements over the linear standard ${\kappa}-{\varepsilon}$. The anisotropic turbulence models predicted turbulence structure in large flow region fairly well but could not predict the very high turbulent intensity of azimuthal velocity observed in narrow flow region(gap).

• 대한조선학회논문집
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• 제60권6호
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• pp.416-423
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• 2023

Recently, the design point of the propeller is gradually changing due to the demand for energy saving and environmental protection. Until recently, self-propulsion model tests were conducted using stock propellers and geometry information was provided to propeller designers, but the range of existing stock propellers did not keep up with the changing design points, and the range of series propellers required in the initial design was also insufficient. Future propeller performance requires high performance and eco-friendliness, and the need for expansion of series propellers has increased. In order to respond to future needs and provide a wide range of advantages in propeller design, KRISO manufactures about 100 series propellers and builds series data through a model tests. In this paper, the approach method for deriving the representative optimal shape to be applied to the 4-blade series propeller in the initial stage of series propeller development was summarized.

• Journal of Advanced Marine Engineering and Technology
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• 제32권5호
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• pp.691-697
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• 2008

Heat exchangers are commonly used in practice in a wide range of application, from heat and air-conditioning system in a household, to chemical processing and power production in large plant. An Experimental study was conducted to investigated the fluid flow and heat transfer around four circular cylinders of in-line in a cross flow of air. The local and average heat transfer characteristics for tube banks are investigated in the present study. Heat transfer in a heat exchanger usually involves convection in each fluid and conduction through the wall separating the two fluid. The in-line pitch ratio was in the range $1.5{\leq}L/d{\leq}4.0$, where L is the center distance and d the cylinder diameter, and in the Reynolds number $8,000{\leq}Re{\leq}50,000$. The local and mean Nusselt numbers were estimated. Subsequently, the heat transfer characteristics of four circular cylinders are found to exhibit a strong dependency upon the separation point of their upstream cylinders.

• 동력기계공학회지
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• 제12권5호
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• pp.48-53
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• 2008

Heat exchangers are commonly used in practice in a wide range of application, from heating and air-conditioning system in a household, to chemical processing and power production in a large plant. Heat transfer in a heat exchanger usually involves convection in each fluid and conduction through the wall separating the two fluids. The heat transfer characteristics of tube banks of in-line arrangements of four circular cylinders in a cross flow are compared for a range of tube locations and Reynolds numbers. The in-line pitch ratio was set up in the range of $1.5\leq L/d\leq4.0$, where L is the center to center distance and d the circular cylinder diameter, and in the Reynolds number of $13,000\leq Re\leq50,000$. The local and mean Nusselt numbers were estimated, and then. Subsequently, the heat transfer characteristics of four circular cylinders were found to exhibit a strong dependency upon the cylinder spacing and separation point of their upstream cylinders.