• Journal of the Korean Society of Propulsion Engineers
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• v.22 no.3
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• pp.28-39
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• 2018

In this study, numerical simulations were performed for steady and unsteady state characteristics of length effects on linear pintle nozzles using the overset grid method. Nozzles and pintles are created separately by an auto grid generation program to use the overset grid method. Appropriate turbulent models and numerical methods are selected for the validation of simulations. Pintle shapes are chosen from five types, with differences in the ratio of length and diameter. The longer the pintle length, the greater the thrust and thrust coefficient. The chamber pressure tendency of steady-state and unsteady-state are different for various pintle velocities. The thrust of the nozzle exit responds to changes in the nozzle throat in the unsteady-state, and the speed of pressure propagation wave generated by movement of the pintle is considered to predict the major factor of performance.

• Proceedings of the KSME Conference
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• 2008.11b
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• pp.2682-2687
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• 2008

Depressurized drainage systems have been used for more than 30 years and are becoming a common part of urban drainage infrastructures. The hydraulic principles governing the operation of the depressurized drainage systems were studied in this paper and particularly, focused on the analysis of unsteady characteristics of the two-phase flow. A definition of the filling ratio was outlined and types of flow pattern were classified according to the filling ratio. Experiments were conducted to investigate the main features of pressure fluctuation. All results were found to depend on the filling ratio of the upstream pipe flow as well as the upstream Froude number.

• Proceeding of EDISON Challenge
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• 2016.03a
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• pp.638-642
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• 2016

현재 양력발생의 원리는 긴 경로 이론과 동시 통과 이론 등으로 알려져 있으며, 이 이론들은 간단히 설명하려는 목적으로 인해 양력발생의 원리가 와전되어왔다. 본 연구에서는 여러 양력발생의 원리 중 Kutta-Joukowski의 이론을 이용하여 순환을 통한 양력발생의 관계에 대해 연구를 수행하였다. 해석 모델은 대칭형 에어포일인 NACA0012를 이용하였다. 해석 프로그램으로는 EDISON을 이용하였으며 시간에 따른 와도를 확인하기 위해 비정상상태 해석을 진행하였다. 그 결과 유동이 시간의 경과에 따라 에어포일 뒷전으로 밀려나면서 Kutta-Joukowski의 이론에 중요한 논점인 출발 와류가 생성됨을 확인할 수 있었다. 이로 인해 순환이 형성되어 양력이 발생함을 추측할 수 있다. 추가적으로 받음각과 출발 와류 사이의 영향성을 연구하였다. 받음각이 커짐에 따라 출발 와류가 에어포일 뒷전에서 더 크게 발생하였고, 받음각이 낮아질수록 출발 와류의 진행이 가속화됨을 확인할 수 있었다.

• Proceedings of the Korean Society of Precision Engineering Conference
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• 2007.06a
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• pp.571-572
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• 2007

• Proceeding of EDISON Challenge
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• 2012.04a
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• pp.105-108
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• 2012

이차원 단면 Cylinder는 외부유동상태에서 후류에 Vortex를 생성한다. 또한 비정상 유동 상태에서는 후류에 카르만 Vortex열을 생성한다. 이런 이차원 Cylinder는 여러 분야에서 사용 된다. 이때 적절한 설계를 위해 수치적으로 유동을 해석할 필요가 있다. 이에 대한 수치적 해석 값을 얻기 위해 Edison CFD를 이용하여 여러 2차원 형상 Cylinder의 Reynolds number에 따른 Vortex shedding을 해석했다. Edison CFD를 통한 시뮬레이션 결과 값에 대한 검증을 얻기 위해 원형, 사각형의 Vortex shedding과 유동을 타 논문과 비교 검증했다. 형상마다 같은 조건의 Reynolds number라도 후류와 유동 등의 형상이 차이를 보인다. 상황마다 적절한 모형의 Cylinder를 Edison CFD를 통해 예측 할 수 있다.

• Proceedings of the Korean Vacuum Society Conference
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• 1993.02a
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• pp.38-40
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• 1993

급속 열처리 시스템내에서의 비정상상태 온도분포, 가스유동형태, 웨이퍼내 열응력등을 여러 가지 작동조건하에서 2차원 유한 차분법으로 계산하였다. 계산결과는 실험에서 얻은 에피성장률 데이터와 비교 검증하였다. RTpp내 가스 유동이나 온도분포는 압력 및 주위 구성요소에 크게 의존하는 반면, 웨이퍼의 온도분포는 wafer edge loss가 큰 고온에서 온도 불균일도가 가장 크다. 저온에서는 대류에 의한 열 손실이 웨이퍼내의 온도 불균일도에 큰 영향을 미치고 있다. 웨이퍼상의 열응력을 가장 크게 받는 시점은 transient condition에서 나타났다.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 1997.04a
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• pp.588-593
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• 1997

본 연구에서는 이전의 연구들이 주로 정상상태의 공력만을 이용하여 소음을 예측하였으나 통상 팬은 단독으로 존재하지 않고 열교환기(radiator)와 같은 주의 물체와 함께 있으므로 이에 따르는 상호작용으로 인한 비정상 유동을 고려하여 소음을 예측하였다.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.19 no.12
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• pp.896-902
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• 2018

This study examined the flow and noise inside a sirocco fan for ventilation as a commercial program. To confirm only the location and power of the noise source, flow analysis was performed with steady state flow analysis. Through flow analysis, the flow was observed in the sirocco fan and the velocity vector. The pressure distribution inside was observed with contours. From the results of steady analysis, the position and size of the noise source could be seen using the 'Curle surface acoustic power' and 'Proudman acoustic power'. The Curle surface acoustic power can be used to observe the noise from the surface. The Proudman acoustic power can be used to detect noise generated in the flow region because the position and size of the noise source generated inside the sirocco fan can be seen only in the steady state. Therefore it is necessary to further analyze the unsteady state to check the frequency of the noise generated. This study provides basic data for improving the performance of the Sirocco fan and reducing the noise.

• Journal of Energy Engineering
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• v.26 no.4
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• pp.67-73
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• 2017

For the bio-fuel conversion of algae, several processes are needed including cultivating, agglomeration, extracting and conversion to the bio-fuel. The production cost for each process makes the total production cost of algae bio-fuel conversion. The production cost of algae bio-fuel has still higher than that of the other commercial bio-fuel. The reduction of production cost for each process enables the competitive price as a bio-fuel. It is difficult to separate the algae from water because of the similar magnitude of density each other. The agglomeration and extracting of algae using ultrasonic wave is rare effect of environmental hazard and also it is appropriate technology for the next generation energy resources. The present research is investigated for the elucidation of algae behavior in the water with the ultrasonics wave. For this purpose, the unsteady computational fluid dynamic analysis has been conducted in the ultrasonic pressure field. The velocity, pressure and algae concentration changes with time have been analysed to clarify the mechanism of algae separation by ultrasonic wave.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2009.05a
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• pp.99-102
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• 2009

LES(Large eddy simulation) of breakup and atomization of a liquid jet into cross turbulent flow was performed. Two phase flow between a gas phase and a liquid phase was modeled by a mixed numerical scheme of both Eulerian and Lagrangian methods for gas and liquid phases respectively. The first and second breakup of liquid column was observed. The penetration depth in cross flow was comparable with experimental data for several variant of a liquid-gas momentum flux ratio by varying liquid injection velocities. SMD(Sauter Mean Diameter) distribution downstream of jet was analyzed.