• Composites Research
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• v.34 no.4
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• pp.233-240
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• 2021

VaRI(Vacuum assisted Resin Infusion) process, which is cost effective and suitable for manufacturing large-sized composites, is an OoA(Out-of Autoclave) process. For rapid resin infusion in the VaRI process, a DM(distribution media) is placed on top of the fabric. The resin is rapidly supplied in plane direction of the fiber along the DM, and then the supplied resin is impregnated in the out-of-plane direction of fiber. It is difficult to predict the flow of resin because the flow of in-plane direction and the out-of-plane direction occur together, and a 3D numerical analysis program is used to simulate the resin infusion process. However, in order to analyze in 3D, many elements are required in the out-of-plane direction of fabric. And the product size is larger, the longer the analysis time needs. Therefore, in this study, a method was suggested to reduce the time required for flow analysis by simplifying the 3D flow analysis to 2D flow analysis. The usefulness was verified by comparing the 3D flow analysis with the simplified 2D flow analysis at the same conditions. The filling time error was about 7% and the reduction of flow analysis time was about 95%. In addition, by utilizing the constant difference in the flow front between the top, middle, and bottom of the fabric of the 3D analysis, the flow front of the top, middle, and bottom of the fabric can be also predicted in the 2D flow analysis.

• Aerospace Engineering and Technology
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• v.11 no.1
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• pp.126-134
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• 2012

The Single Species, Unreacted Flow Model which is effectively applicable on the computational analysis of rocket exhaust flow is introduced in this paper. The basic concept of this model had been originated from chemically frozen analysis of hot air but it was complemented by compensating molecular weight and specific heat which was obtained CEA code analysis of exhaust plume. Comparing single species, unreacted model with the finite chemistry model, unreacted model can reduce calculation time to 1/5 while it makes similar simulation results.

• 한국전산유체공학회:학술대회논문집
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• 1999.05a
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• pp.131-136
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• 1999

박리를 수반하는 진동하는 이차원 익형 주위의 비정상 유동장에 대해 SST 난류 모델을 이용하여 해석을 수행하였다. SST 모델은 정상 유동장 해석에서 기존의 난류 모델에 비해 우수한 성능을 보인다고 알려져 있으나 큰 박리영역에서 공력 계수의 진동 현상을 보이는 등 비정상 유동장 해석에 문제점을 보이고 있다. 본 논문에서는 이러한 공력 계수의 진동 현상이 SST 모델을 이차원으로 확장하는 과정에서 발생한 것임을 밝히고 이에 대한 보완을 통하여 수정된 SST 모델을 제시하고자 한다. SST 모델의 기본이 되었던 BSL 모델 및 SST 모델, 수정된 SST 모델을 사용하여 정상 유동장과 비정상 유동장 해석을 수행하여 각 모델의 난류 유동장 해석 특성을 비교하고 이를 통하여 수정된 SST 모델이 박리를 수반하는 비정상 유동장 해석에서 원래의 SST 모델에 비해 향상된 결과를 나타남을 알 수 있었다.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2009.05a
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• pp.369-372
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• 2009

A numerical analysis of the effect of plasma on flow characteristics in supersonic flow is studied. It is shown that change of direction and velocity magnitude of flow is appeared different in relative direction of plasma and fluid flow. The case of that direction of electrons, which are same with flow direction, the flow is accelerated, and the case of opposition, the flow is decelerated.

• Proceedings of the Korea Society for Energy Engineering kosee Conference
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• 1995.11a
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• pp.5-14
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• 1995

본 연구는 석탄가스화기내의 비반응 유동장에 대한 연구로서, 순수유동장 및 미분탄입자를 포함한 이상유동장에 대한 전산해석을 수행하였다. 가스화기내의 물리적 현상을 기술하는 Navier-Stokes 방정식을 유한차분법에 의하여 해석하고 그 결과를 나타내었다. 특히 선회유동의 영향에 의한 미분탄입자의 거동 및 재순환영역의 특성에 대하여 상세히 고찰하였다. 해석결과에 의하면 가스화기내에서는 몇개의 재순환영역이 형성됨을 알 수 있었다. 비반응유동장의 해석결과이지만, 선회유동은 화염안정화에 긍정적인 영향을 줄 수 있을 것으로 추측되는 결과를 보였다.

• Journal of the Korea Convergence Society
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• v.11 no.1
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• pp.195-200
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• 2020

In this study, the flow analyses by type of shock absorber orifice were carried out. A shock absorber is indispensable for the ride comfort that is important at the standard of a good car. As the analysis procedure, the actual speed of the shock absorber was set as the flow rate when the cylinder was advanced. And the flow analysis results on models A, B and C of shock absorber models were compared with each other. As the examination on the flow orifice in the vicinity of each model through the analysis of flow, the performance of shock absorber were recognized. On the whole, model A had the fastest flow rate and also had the largest flow rate. Model B had the slowest flow rate and the flow rate features of models B and C with the same number of orifices were similar. Through this study, it is possible to see which shock absorber orifice model facilitates the flow inside the cylinder and increases the ride comfort. It is seen that this analysis result on the flow analyses by type of shock absorber orifice can be applied by converging with the field of design.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.35 no.8
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• pp.677-684
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• 2007

In the Present Study, a 3-D viscous flow solver, based on unstructured hybrid meshses containing tetrahedra, prisms and pyramids, has been developed. A finite-volume discretization scheme is used for solving the compressible Navier-Stokes equations. A cell-vertex median dual volume is used for spatial discretization. The one-equation Spalart-Allmaras turbulence model has been adopted to evaluate the eddy viscosity. Validation were made by computing laminar and turbulent flows around a 3-D wing for steady flows and turbulent flows around an oscillating 3-D wing in harmonic motion for unsteady flows.

• Proceedings of the KAIS Fall Conference
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• 2002.11a
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• pp.253-257
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• 2002

This study is object to flow analysis of ice cone die. The finite element model was developed to compute the flow, velocity and pressure for ice cone die. For flow analysis using result from FEM Code.

• Proceedings of the KAIS Fall Conference
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• 2009.12a
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• pp.511-514
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• 2009

현재 일반적으로 사용되는 300cc 소형엔진 기화기의 최적화 및 성능 향상을 위하여 유동해석을 수행하였다. 베르누이의 정리를 기본으로, 성능을 발휘하는 주요 설계인자인 기화기 내부의 벤튜리 튜브의 각도, 길이 등을 변수로 하여 유동해석을 수행하였다. 그 결과를 분석하여 최적화된 모델을 제시하였다. 결론적으로, 유동 해석을 바탕으로 기존 사양 대비 향상된 성능의 모델을 제시하였다. 유동해석을 통해 기화기 내부의 벤튜리관에 곡면(Rounding)처리를 적용함으로 기화기에서 소모되는 흡기저항을 줄여 펌핑로스를 저감활수 있음을 확인하였다. 펌핑로스의 저감은 엔진 연비의 향상과 엔진토크에 긍정적 효과로 작용할 것으로 기대된다. 벤튜리관의 출구 각도를 감소시킴으로 박리를 개선하여 Dead Volume을 줄임으로서 기존 모델에 대비하여 원활해진 유동의 흐름을 얻을 수 있었다. 이는 흡기유량을 증대시키고 엔진출력을 상승시키는 효과로 작용할 것으로 예상된다.

• The Journal of the Korea Contents Association
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• v.18 no.6
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• pp.27-37
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• 2018

Streamline generation is one of the most representative visualization methods to analyze the flow stream of fluid dynamics dataset. It is a challenging problem, however, to determine the seed locations for effective streamline visualization. Meanwhile, it needs much time to compute effective seed locations and streamlines on the massive flow dataset. In this paper, we propose not only an importance based method to determine seed locations for the effective streamline placements but also a parallel streamline visualization method on the distributed visualization system. Moreover, we introduce case studies on the real fluid dynamics dataset using GLOVE visualization system to evaluate the proposed method.