• Journal of computational fluids engineering
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• v.9 no.1
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• pp.41-47
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• 2004

A successful store separation analysis tool, MSAP(Multi-body Separation Analysis Program) has been applied to F/A-18C/JDAM CFD Challenge Ⅱ. The challenge was devised to challenge CFD community to use CFD methodologies to predict and match the trajectory of a JDAM MK-84 separating from F/A-l8C. Trajectory simulations for two flight conditions were performed. Comparison between computed and measured flight trajectories for both conditions shows a good agreement.

• Proceedings of the Korean Society for Bio-Environment Control Conference
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• 2001.11a
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• pp.78-81
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• 2001

포그냉방시스템에 관한 연구는 대부분 VETH선도 등을 이용하여 온실 환경이 전체적으로 동질이라는 가정하에서 환기량 및 전체 분무수량 등을 계산하는 정도였으나, 1990년대 중반에 들어서면서 CFD 기법을 이용하여 온실 환경을 보다 정확하게 해석할 목적으로 CFD 기법을 이용하는 연구가 활발하게 이루어지고 있다. (중략)

• 한국전산유체공학회:학술대회논문집
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• 2001.10a
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• pp.37-43
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• 2001

The methods of atmospheric boundary layer generation in test section were reviewed. To utilize conventional aerodynamic wind tunnels as atmospheric wind tunnels, boundary layer growth should be accelerated. To achieve this, improvement of boundary layer generation devices is required and it might be done by CFD. In this respect, CFD application cases in boundary generation devices were reviewed and potential areas were considered. Some cases are tried by Fluent 5 code.

• Proceedings of the Korean Society for Bio-Environment Control Conference
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• 2000.10b
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• pp.80-83
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• 2000

최근에 CFD 시뮬레이션을 이용한 온실의 공기유동을 해석하려는 시도들이 많이 이루어지고 있다. 그러나 아직 열환경까지를 해석하려는 경우는 드물다. 그러나 여름철의 고온극복을 위해 많은 냉방시스템이 연구되고 있는데 이러한 것들의 이용에 있어서 CFD 시뮬레이션을 이용한 열환경 해석은 중요한 의미를 가질 것이다. 그리고 여러 가지 냉방시스템들 중에서 포그시스템이 효율, 경제적 측면에서 유리하다고 알려져 있다. (중략)

• 한국전산유체공학회:학술대회논문집
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• 2004.10a
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• pp.105-109
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• 2004

CFD simulation for Smart-UAV(TR-E2Sl) is performed to analyze its aerodynamic characteristics. Base geometry and several cases, decided by control surfaces being deflected, are simulated. To obtain the better lift characteristics, the elevator should be deflected between 10o and 20o with the incidence angle of the wing 1o.

• Journal of the Korean Society of Visualization
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• v.2 no.2
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• pp.20-24
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• 2004

Recent advances in CFD technique along with a rapid growth of computer resources provide valuable opportunities for developing an accurate way of visualizing turbulent structures. Not only this visualization technique made it possible to check the validity of many of theoretical achievements of the past but also it pushes the current turbulence research to a new paradigm. A brief history of visualization study will be summarized and discussed.

• 한국전산유체공학회:학술대회논문집
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• 2005.04a
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• pp.114-118
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• 2005

CFD simulation was peformed for 2D and 3D flying and rotating frisbees. Multiple reference method(MRF) was utilized to consider the rotation of 3D model. Geometry change of 2D model shows dramatic increase of lift, but 3D simulation results for geometry change show decrease of lift and drag. Ground effect increases the lift of the frisbee being close to ground.

• 한국전산유체공학회:학술대회논문집
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• 2011.05a
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• pp.350-355
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• 2011

The hot gas reingestion phenomenon of helicopter brings about the reduction of engine power available around in-ground. The phenomenon will vary for the conditions of ambient conditions and engine exhaust gas, the flow field associated with the downwash effect of main rotor. To verify the amount of hot gas reingestion to intake, Tests(Wind tunnel test, Flight test) or CFD could be available. At this study, the reingestion around in-ground would be predicted by numerical analysis(CFD).

• Korea-Australia Rheology Journal
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• v.21 no.3
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• pp.161-173
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• 2009

This study analyzes especially drag and lift models recently developed for fluid-solid, fluid-fluid or liquid-liquid two-phase flows to understand their applicability on the computational fluid dynamics, CFD modeling of pulsatile blood flow. Virtual mass effect and the effect of red blood cells, RBCs aggregation on CFD modeling of blood flow are also shortly reviewed to recognize future tendencies in this field. Recent studies on two-phase flows are found as very useful to develop more powerful drag-lift models that reflect the effects of blood cell's shape, deformation, concentration, and aggregation.

• Proceeding of EDISON Challenge
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• 2014.03a
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• pp.659-662
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• 2014

본 연구에서는 전산유체 해석프로그램인 EDISON_CFD를 이용하여 Clark-Y 에어포일의 공력특성 변화를 수치해석하고, 여러 가지 받음각의 변화를 통해 양력계수, 항력계수, 양항비 등을 도출하였다. 공력해석을 위한 조건으로 압축성 Navier-Stokes 방정식에 난류 유동조건을 적용하였다. 해석 결과는 에어포일 공력해석 툴로 널리 알려져 있는 XFOIL을 이용하여 비교 검토하였다.