• 유기물자원화
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• 제14권3호
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• pp.85-90
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• 2006

플라즈마 용융로에 설치된 폐열 보일러를 실측치와 근접한 모의 보일러를 설계하여 CFD(전산유체역학) 프로그램을 이용하여 얻어진 보일러 내에서의 유해가스발생 및 열 유동현상에 대한 열 설계 능력 확보와 폐열보일러 효율 개선에 대한 연구를 수행하는데 목적이 있다. 보일러 내에서의 온도변화 및 연소가스의 공기 유동, 부식성 가스의 영향으로 인해 보일러 내부에서의 부식위치 및 클링커 생성여부에 관한 연구를 통해 효율적인 보일러의 구조 설계 및 에너지 재활용방안에 이용하고자 한다. 연구결과 플라즈마 용융로에 설치된 보일러 설비는 2차 연소로 출구에서 배출되는 약 $1,200^{\circ}C$의 연소가스를 약 $450^{\circ}C$까지 냉각시킬 수 있는 설계조건을 만족시켰다. 반면 유해가스 유동 결과 보일러 입구 부분의 상단부와 하단부에 부식성 가스 (SOx, HCl)의 영향으로 인하여 부식 및 클링커 생성이 보일러의 다른 위치보다 쉽게 발생될 것으로 예상된다. 이로 인해 보일러 내 외관벽의 부식으로 보일러의 수명 단축 및 효율적인 폐열을 재활용 할 수 없다고 예상된다. 이에 따른 저온 및 고온 부식 방지대책에 대한 세심한 고려가 필요하다 하겠다.

• 한국화재소방학회논문지
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• 제29권5호
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• pp.42-50
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• 2015

도심지역을 단순 모델링한 실규모 공간에서 누출된 프로판 확산과정에 대해 대와동모사(Large Eddy Simulation: LES), 분리와동모사(Detached Eddy Simulation: DES) 및 비정상 레이놀즈평균기법(Reynolds Averaged Navier-Stokes: RANS)을 이용한 3가지 전산해석을 수행하였다. 전산해석은 FLUENT 14를 이용하였고 격자계는 ICEM-CFD를 이용하여 구성하였다. 그 결과 건물 주변의 프로판 농도분포는 주변 와구조와 밀접한 관련이 있어 이러한 와구조를 합리적으로 예측하는 정도에 따라 농도분포가 크게 차이날 수 있음을 알았다. LES와 DES는 비교적 유사한 와구조와 프로판 농도분포를 보이지만 RANS는 너무 부드러운 농도분포를 보여 복잡한 비정상적인(Unstedy) 난류 유동장을 재현하는데 한계가 있어 가스연료 누출 초기의 농도분포 전개과정을 예측하는 데에는 어려움이 있을 것으로 판단된다. 해석결과와 계산시간까지 고려한다면 DES 방법이 실규모에서의 가스연료 누출 확산과정에 대한 CFD 해석방법으로 적합할 것으로 판단된다.

• 한국항공우주학회지
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• 제47권1호
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• pp.17-25
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• 2019

항공기의 Intake는 공간적 제약 또는 생존성 확보의 이유로 S형태의 곡률을 갖는 덕트를 가진다. 그러나 덕트의 곡률은 2차유동과 유동박리의 발생을 야기하며 불균일한 압력분포 생성의 원인이 된다. 본 연구에서는 RAE M 2129 S-Duct의 형상에 보조 Duct를 적용하여 경계층 흡입을 수행하였다. 경계층 흡입의 위치와 각도를 설계변수로 설정하였으며, 흡입면에서 동일 유량을 흡입하는 조건을 부여하였다. S-Duct의 전산해석 타당성을 검증하기 위하여 Port Side와 Starboard Side의 무차원 압력 분포를 ARA 실험값, 전산해석 값과 각각 비교하여 확인하였다. 본 연구에서는 유동 왜곡을 판단하는 공기역학적 성능인자로 유동 왜곡 계수를 사용 하였으며, 경계층 흡입에 의한 유동박리, 와류, 유량 분포 및 압력 분포를 비교 분석 하였다. 그 결과 경계층 흡입 적용 이전과 비교하여 최대 26.14%의 유동 왜곡 계수 저감 효과를 확인하였다.

• 한국해양공학회지
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• 제35권1호
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• pp.50-58
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• 2021

The demand for eco-friendly energy is expected to increase due to the recently strengthened environmental regulations. In particular, the flow inside the pipe used in a cargo handling system (CHS) or fuel gas supply system (FGSS) of hydrogen transport ships and hydrogen-powered ships exhibits a very complex pattern of multiphase-thermal flow, including the boiling phenomenon and high accuracy analysis is required concerning safety. In this study, a feasibility study applying the boiling model was conducted to analyze the multiphase-thermal flow in the pipe considering the phase change. Two types of boiling models were employed and compared to implement the subcooled boiling phenomenon in nucleate boiling numerically. One was the "Rohsenow boiling model", which is the most commonly used one among the VOF (Volume-of-Fluid) boiling models under the Eulerian-Eulerian framework. The other was the "wall boiling model", which is suitable for nucleate boiling among the Eulerian multiphase models. Moreover, a comparative study was conducted by combining the nucleate site density and bubble departure diameter model that could influence the accuracy of the wall boiling model. A comparison of the Rohsenow boiling and the wall boiling models showed that the wall boiling model relatively well represented the process of bubble formation and development, even though more computation time was consumed. Among the combination of models used in the wall boiling model, the simulation results were affected significantly by the bubble departure diameter model, which had a very close relationship with the grid size. The present results are expected to provide useful information for identifying the characteristics of various parameters of the boiling model used in CFD simulations of multiphase-thermalflow, including phase change and selecting the appropriate parameters.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2006년도 PARALLEL CFD 2006
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• pp.395-397
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• 2006

Air interlacing serves to protect the yarn against damage, strengthens inter-filament compactness or cohesion, and ensures fabric consistency. The air interlacing nozzle is used to introduce intermittent nips to a filament yarn so as to improve its performance in textile processing. The effect of various interlacing nozzle geometries on the interlacing process was studied. The geometries of interlacing nozzles with single or multiple air inlets located across the width of yarn channels are investigated. The basis case is the yarn channel, with a perpendicular main air inlet in the middle. Other cases have main air inlets, slightly inclined double sub air inlets, The yarn channel cross sectional shapes are either semicircular or rectangular shapes. The compressed impinging jet from the main air inlet hole hits the opposing bottom wall of the yarn channel, is divided into two branches, joins with the compressed air coming out from sub air inlet at the bottom and creates two free jets at both ends of the yarn channel. The compressed air movement in the cross-section consists of two opposing directional vortices. The CFD-FASTRAN flow parallel solver was used to perform steady simulations of impinging jet flow inside of the interlace nozzles. The vortical structure and the flow pattern such as pressure contour, particle traces, velocity vector plots inside of interlace nozzle geometry are discussed in this pater.

• 한국항공우주학회지
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• 제46권9호
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• pp.703-711
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• 2018

본 연구에서는 실기체 환경 모사(고도 모사)가 가능한 극초음속 Ludwieg tube 개념설계 도구를 개발하고, 전산유체해석을 통해 Ludwieg tube 개념설계 도구의 성능을 검증하였다. 극초음속 Ludwieg tube 개념설계 도구를 개발하기 위해 Ludwieg tube의 작동원리를 연구하였고, 도구를 활용하여 목표 성능을 만족하기 위한 Ludwieg tube의 제원을 결정하였다. 마하수 4에서 10의 유동을 모사할 수 있고, 특히 마하수 4 유동은 고도 모사가 가능하다.

• International Journal of Naval Architecture and Ocean Engineering
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• 제13권1호
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• pp.858-876
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• 2021

Although widely used, the design of the bulbous bow for ships has been difficult due to the complex interference between the wave system generated by the bulb and the wave system of the ship hull. Until now, a bulbous bow has been often designed using Kracht charts, which were established based on model test data, but these charts apply only to ships with a block coefficient C_B = 0.56-0.82, Froude number Fn = 0.20-0.40, and the obtained bulb sizes are only close to optimal. This paper presents a new method for the optimal design of bulbous bow, starting from the design of an initial bulb using Kracht charts for ships with any block coefficient or Froude number, then resizing this initial bulb to define the optimal bulb sizes based on a multi-objective function of the required power reduction, and a combined solution of Computation Fluid Dynamics (CFD) analysis and surrogate models. This study was applied to a fishing vessel FAO 75, which has been model tested and used to design steel fishing vessels in Vietnam recently. The obtained quantitative results showed the same trend as the theory and practice, with a reduction of the ship's required power by about 14%.

• 한국전산유체공학회지
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• 제20권1호
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• pp.10-15
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• 2015

In this study, the characteristics of water treatment mixer with various propeller profiles are numerically invesitgated. The computation was conducted by solving the incompressible Navier-Stokes equations on unstructured tetrahedral elements with k-${\varepsilon}$ turbulence model. It was found that the spreading angle and swirl magnitude of the jet are important factors for the mixer efficiency, since they clearly characterize the propeller and the frontal surface area of the propeller but not so much affected by the skew angle if it exceeds 30 degrees. The case1 and case2 models are found to show the best propeller efficiency. The case2 with low blade angle, however, requires the lowest power input for the same discharge capacity as the case1.

• 한국정밀공학회지
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• 제29권9호
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• pp.1003-1011
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• 2012

A new type of gerotor developed in this paper has the inner rotor designed by inserting a polycircular-arc between the hypocycloid and epicycloid curves, and we also suggest that the outer rotor be designed using the closed-form equation for the inner rotor and a method of modification. Thus, it is possible to design a gerotor for which there is no cusp and loop, as in this case undercut is prevented. We developed automated program for rotor design and calculation of the flow rate and flow rate irregularity. And we also demonstrate the superior performance of the gerotor developed in this study by analyzing the internal fluid flow using a commercial computation fluid dynamics-code (CFD).

• Advances in Computational Design
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• 제6권1호
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• pp.31-42
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• 2021

This research aims to demonstrate the optimal geometrical design of splayed multiple cross-sectional pin fin heat sinks (SMCSPFHS), which are a type of side-inlet-side-outlet heat sink (SISOHS). The optimiser strength Pareto evolutionary algorithm2 (SPEA2)is employed to explore a set of Pareto optimalsolutions. Objective functions are the fan pumping power and junction temperature. Function evaluations can be accomplished using computational fluid dynamics(CFD) analysis. Design variablesinclude pin cross-sectional areas, the number of fins, fin pitch, thickness of heatsink base, inlet air speed, fin heights, and fin orientations with respect to the base. Design constraints are defined in such a way as to make a heat sink usable and easy to manufacture. The optimum results obtained from SPEA2 are compared with the straight pin fin design results obtained from hybrid population-based incremental learning and differential evolution (PBIL-DE), SPEA2, and an unrestricted population size evolutionary multiobjective optimisation algorithm (UPSEMOA). The results indicate that the splayed pin-fin design using SPEA2 issuperiorto those reported in the literature.