• 한국자동차공학회논문집
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• 제1권1호
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• pp.32-40
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• 1993

Flow fields in model engine cooling passages are studied numerically by using TURBO-3D program, a finite volume based 3-D turbulent flow program adopting a general body fitted coordinate system. The effects of exit position on mass flow rate at each gasket hole are examined for a model cooling passage in order to understand the flow distribution inside the water jacket. The results of the present study can be applied to the design of high performance, high reliability engine.

• Advances in aircraft and spacecraft science
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• 제7권3호
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• pp.203-214
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• 2020

In many applications like the aircraft or the rockets/missiles, the flow from a nozzle needs to be expanded suddenly in an enlarged duct of larger diameter. The enlarged duct is provided after the nozzle to maximize the thrust created by the flow from the nozzle. When the fluid is suddenly expanded in an enlarged duct, the base pressure is generally lower than the atmospheric pressure, which results in base drag. The objective of this research work is to optimize the length to diameter (L/D) ratio of the enlarged duct using the CFD analysis in the flow field from the supersonic nozzle. The flow from the nozzle drained in an enlarged duct, the thrust, and the base pressure are studied. The Mach numbers for the study were 1.5, 2.0 and 2.5. The nozzle pressure ratios (NPR) of the study were 2, 5 and 8. The L/D ratios of the study were 0.5, 1, 2, 3, 4, 5, 6, 7, 8, 9 and 10. Based on the results, it is concluded that the L/D ratio should be increased to an optimum value to reattach the flow to an enlarged duct and to increase the thrust. The supersonic suddenly expanded flow field is wave dominant, and the results cannot be generalized. The optimized L/D ratios for various combinations of flow and geometrical parameters are given in the conclusion section.

• 유체기계공업학회:학술대회논문집
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• 유체기계공업학회 2002년도 유체기계 연구개발 발표회 논문집
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• pp.396-401
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• 2002

The purpose of this 3-D numerical simulation is evaluate the application of a commercial CFD code to predict 3-D flow characteristics of wind turbine. The experimental approach, which has been main method of investigation, appears to be its limits, the cost increasing disproportionally with the size of the wind turbines, and is hence mostly limited to observing the phenomena. Hence, the use of Computational Fluid Dynamics (CFD) techniques and Wavier-Stokes solvers are considered a very serious contender. The flow solver CFX-TASCflow is employed in all computations presented in this paper. The 3-D flow separation and the wake distribution of 2 bladed Horizontal Axis Wind Turbines (HAWTs) are compared to Heuristic model and visualized result by NREL(National Renewable Energy Laboratory). Simulated 3-D flow separation structure on the rotor blade is very similar to Heuristic model and the wake structure of the wind turbine is good agree with visualized results.

• 한국콘텐츠학회논문지
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• 제12권1호
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• pp.166-175
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• 2012

<나탈리>(2010)와 <7광구>(2011)를 통해 한국 3D 영화제작의 가능성이 확인됐다. 그러나 동시에 한국 3D 영화제작 환경에서의 다양한 기술적, 제작과정상의 문제점이 도출되었다. 본 연구는 <7광구>의 3D 영화제작 사례를 분석한 결과이다. 분석은 주로 기술적인 오류와 제작 공정상의 파이프라인에서 드러난 문제점에 주목하여 이루어 졌다. <7광구>를 통해 얻은 제작 경험과 시행착오를 분석함으로써 향후 제작될 한국형 3D 영화의 제작진들에게 실무적인 연구결과를 전달하는 것이 본연구의 목적이다. 분석결과 <7광구>는 기술적인 완성도뿐만 아니라 효율적인 제작 파이프라인 구축에도 실패한 것으로 드러났다. 그럼에도 불구하고 <7광구>는 한국적인 3D 제작공정을 능동적으로 구축하려했다는 점에서 긍정적으로 평가 받는다.

• 한국수자원학회:학술대회논문집
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• 한국수자원학회 2005년도 학술발표회(1)
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• pp.121-122
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• 2005

• 한국산학기술학회논문지
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• 제12권4호
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• pp.1897-1903
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• 2011

본 논문은 2D/3D 변환을 위한 객체 추출과 깊이정보(Depth-map) 생성기법에 관한 연구이다. 2D영상을 3D로 변환하기 위해서는 영상 객체 추출, 영상 거리 인식, 영상 생성, 재보정 단계를 거치게 되는데 본 논문에서는 영상 객체 추출과 영상 거리 인식에 해당하는 깊이정보를 생성하는 방법을 제안한다. 3D 영상으로의 변환은 2D 영상에서의 객체 추출과, 추출된 객체와 주변 배경을 구별하기 위한 거리감을 할당하는 깊이정보 생성이 중요하다. 보다 정확한 객체 추출과 깊이정보를 생성하기 위해 기존의 Optical flow에서 잡음을 제거한 방법을 제안하였다. 제안한 방법으로 2D 영상을 깊이정보가 포함된 영상으로 변환하여 영상의 깊이 정보가 추정됨을 알 수 있다.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2003년도 춘계학술대회
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• pp.2192-2197
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• 2003

The purpose of this 3-D numerical simulation is evaluate the application of a commercial CFD code to predict 3-D flow and power characteristics of wind turbines. The experimental approach, which has been main method of investigation, appears to be its limits, the cost increasing with the size of the wind turbines, hence mostly limited to observing the phenomena on rotor blades. Therefore, the use of Computational Fluid Dynamics (CFD) techniques and Navier-Stokes solvers are considered a very serious contender. The flow solver CFX-TASCflow is employed in all computations in this paper. The 3-D flow separation and the wake distribution of 2 and 3 bladed Horizontal Axis Wind Turbines (HAWTs) are compared to Heuristic model and smoke-visualized experimental result by NREL(National Renewable Energy Laboratory). Simulated 3-D flow separation structure on the rotor blade is very similar to Heuristic model and the wake structure of the wind turbine is good consistent with smoke-visualized result. The calculated power of the 3 bladed rotor by CFD is compared with BEM results by TV-Delft. The CFD results of which is somewhat consist with BEM results, under an error less than 10%.

• Journal of Advanced Marine Engineering and Technology
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• 제27권7호
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• pp.906-913
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• 2003

The purpose of this 3-D numerical simulation is to evaluate the application of a commercial CFD code to predict 3-D flow and power characteristics of wind turbines. The experimental approach, which has been main method of investigation, appears to be its limits, the cost increasing with the size of the wind turbines, hence mostly limited to observing the phenomena on rotor blades. Therefore. the use of Computational Fluid Dynamics (CFD) techniques and Navier-Stokes solvers are considered a very serious contender. The flow solver CFX-TASCflow is employed in all computations in this paper. The 3-D flow separation and the wake distribution of 2 and 3 bladed Horizontal Axis Wind Turbines (HAWTs) are compared to Heuristic model and smoke-visualized experimental result by NREL(National Renewable Energy Laboratory). Simulated 3-D flow separation structure on the rotor blade is very similar to Heuristic model and the wake structure of the wind turbine is good consistent with smoke-visualized result. The calculated power of the 3 bladed rotor by CFD is compared with BEM results by TU-Delft. The CFD results of which is somewhat consist with BEM results. under an error less than 10%.

• 한국기계가공학회지
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• 제17권4호
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• pp.64-69
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• 2018

This paper investigates the compressive deformation behavior of direct metal tooling (DMT), processing titanium alloy (Ti-6Al-4V) parts under high strain loading conditions. Split Hopkinson Pressure Bar (SHPB) experiments were performed to determine the flow stress and the coefficients of the Johnson-Cook model. This model is described as a function of strain, strain rate, and temperature. SHPB experiments were performed to characterize the deformation behavior of specimens made with 3D printers, using Ti-6Al-4V material under high temperature and dynamic loading.

• 한국해안·해양공학회논문집
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• 제26권3호
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• pp.140-148
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• 2014

고조방파제는 폭풍해일이나, 대조시 창조류로부터 내부 해역을 보호하기 위하여 설계된 특수한 형태의 수문 구조물로, 홍수 방지 벽, 방조제 및 다른 구조물로 구성된다. 평상시 고조방파제는 해수 소통을 허용하지만, 폭풍해일이 예상되면 폐쇄된다. 폐쇄시키는 다양한 방법 중 본 연구에서는 이태리 모세프로젝트에 적용한 것과 같은 부유 플랩형 고조방파제를 마산만에 적용할 경우, 폭풍해일 및 파랑이 작용할 때의 고조방파제 거동특성을 3차원 유동해석프로그램인 FLOW-3D를 이용하여 살펴보았다. 수치해석결과, 고조차 2 m인 상태에서 파고 3 m 조건에서도 고조방파제로서의 기능을 발휘할 수 있는 것으로 평가되었다.