• 한국전산유체공학회지
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• 제15권3호
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• pp.54-59
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• 2010

A parametric study has been carried out to elucidate the characteristics of channel flow with a streamwise-periodic array of cylinders. This flow configuration is relevant to heat exchanger applications. The presence of cylinders in channel flow causes the attached wall boundary layer to separate, leading to significant change in flow instabilities. There exist two kinds of instabilities; flow undergoes a primary instability (Hopf bifurcation) at a lower Reynolds number, and the unsteady two-dimensional flow becomes unstable to three-dimensional disturbances at a higher Reynolds number. We report here the dependencies of the primary instability as well as the flow characteristics of the subsequent unsteady flow, including flow-induced forces and Strouhal number of vortex shedding, on the distance between the cylinder and the channel wall.

• 대한전자공학회:학술대회논문집
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• 대한전자공학회 2000년도 하계종합학술대회 논문집(5)
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• pp.187-190
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• 2000

We presents the construction of radio frequency pad area array package modules which operate at radio frequency of 224MHz, and proposes the structure of RF module packages to improve its electrical characteristics. The module of RF PAA package was constructed in the configuration of three dimensional stacked package and reduced size. RF PAA packages showed the optimized and improved gain of 2dB by partitioning the RF transceiver with 3 dimensional stacked PAA packages.

• International Journal of Aeronautical and Space Sciences
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• 제4권1호
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• pp.45-52
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• 2003

A three-dimensional aerodynamic shape optimization technique in inviscid compressible flows is developed by using a parallel continuous adjoint formulation on unstructured meshes. A new surface mesh modification method is proposed to overcome difficulties related to patch-level remeshing for unstructured meshes, and the effect of design sections on aerodynamic shape optimization is examined. Applications are made to three-dimensional wave drag minimization problems including an ONERA M6 wing and the EGLIN wing-pylon-store configuration. The results show that the present method is robust and highly efficient for the shape optimization of aerodynamic configurations, independent of the number of design variables used.

• 대한전기학회논문지:전기물성ㆍ응용부문C
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• 제51권2호
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• pp.80-84
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• 2002

This paper presents some of the results of current research on 400kN Suspension Insulator Design. In this paper, authors carried out 2-dimensional field calculation in order to analyse dielectric characteristics of the insulator unit and 3-dimensional field calculation in order to analyse dielectric characteristics of the insulator strings. And the results of puncture tests of insulators were compared with the required field intensity of the insulator As results, it was found that electric field on the insulator unit is severest between two triple junctions, dielectric characteristics of insulator strings are much influenced by the surrounding configuration and the manufactured insulators have good results of puncture tests.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2001년도 춘계학술대회논문집E
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• pp.690-695
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• 2001

The three-dimensional spatial structures of impeller flow created by a six bladed Rushton turbine have identified based on the volumetric velocity information from multi-plane stereoscopic PIV measurements. A total of 10 planes with 2 mm space with a 50 mm by 64 mm size of the field of view were targeted. To reduce the depth of focus, we adopted an angle offset configuration which satisfied the Scheimpflug condition. The distortion compensation procedure was utilized during the in situ calibration. Phase-locked instantaneous data were ensemble averaged and interpolated in order to obtain mean 3-D, volumetric velocity fields on a 60 degree sector of a cylindrical ring volume enclosing the turbine blade. Using the equi-vorticity surface rendering, the spatial structure of the trailing vortices was clearly demonstrated. Detail flow characteristics of the radial jet reported in previous studies of mixer flows were easily identified.

• 한국의학물리학회지:의학물리
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• 제8권2호
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• pp.27-34
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• 1997

방사선치료에서 three dimensional conformal radiation therapy (3DCRT) 에 접근하는 방법으로 조사하는 방향에 따라 선량의 강도를 조절함으로서 암조직에만 집중적으로 선량을 조사하며 주위 정상조직에는 최소의 선량이 조사되도록 하는 방법으로 1990년대부터 Memorial Sloan-Kettering Cancer Center를 중심으로 연구되었다. 암조직의 치료부피를 최적화하기 위하여 암조직의 모양에 따라 선량분포곡선이 이루는 치료용적이 종양용적과 같아야 한다. 이러한 3DCRT는 암조직에 집중적으로 선량을 조사할 수 있어서 중요장기들의 한계선량을 유지하면서 암조직에 조사되는 선량을 20％ 정도 증가시킬수 있다. 방사선치료의 궁극적인 목적이 종양부위에 균등한 치유선량이 도달되게하고 병변 부위의 정상조직의 손상을 최소가 되게 하는 것이며, 이러한 수행을 위하여 CT planning 등을 이용하여 치료계획을 수립하여 치료용적과 종양용적을 거의 같게 할 수 있다. 본 연구에서는 조사하는 부위에서 선량의 강도를 조절하여 암조직의 치료용적을 최적화하는 3DCRT를 얻는 것을 목적으로 폐암환자에서 강도 조절법을 사용한 치료계획에서 일반적인 치료계획을 시행한 경우를 비교하면 종양용적에 접근한 치료계획과 정상조직에 대한 선량 감소를 보여주고 있으며, 직장암 환자에서도 두 치료계획에서 선량분포가 잘 비교가 됨을 볼 수 있다.

• 대한기계학회논문집B
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• 제27권6호
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• pp.773-780
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• 2003

The three-dimensional spatial structures of impeller flow created by a six bladed Rushton turbine have identified based on the volumetric velocity information from multi-plane stereoscopic PIV measurements. A total of 10 planes with 2 mm space and a 50 mm by 64 mm size of the field of view were targeted. To reduce the depth of focus, we adopted an angle offset configuration which satisfied the Scheimpflug condition. The distortion compensation procedure was utilized during the in situ calibration. Phase-locked instantaneous data were ensemble averaged and interpolated in order to obtain mean 3-D. volumetric velocity fields on a 60 degree sector of a cylindrical ring volume enclosing the turbine blade. Using the equi-vorticity surface rendering, the spatial structure of the trailing vortices was clearly demonstrated. Detail flow characteristics of the radial jet reported in previous studies of mixer flows were easily identified.

• Current Optics and Photonics
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• 제3권1호
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• pp.16-21
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• 2019

We present a broad-bandwidth comb-spacing-swept source (CSWS) based on a differential polarization delay line (DPDL) for interferometric three-dimensional (3D) imaging. The comb spacing of the CSWS is repeatedly swept by the tunable DPDL in the multiwavelength source to provide depth-scanning optical coherence tomography (OCT). As the polarization differential delay of the DPDL is tuned from 5 to 15 ps, the comb spacing along the wavelength continuously varies from 1.6 to 0.53 nm, respectively. The wavelength range of various semiconductor optical amplifiers and the cavity feedback ratio of the tunable fiber coupler are experimentally selected to obtain optimal conditions for a broader 3-dB bandwidth of the multiwavelength spectrum and thus provide a higher axial resolution of $35{\mu}m$ in interferometric OCT imaging. The proposed CSWS-OCT has a simple imaging interferometer configuration without reference-path scanning and a simple imaging process without the complex Fourier transform. 3D surface images of a via-hole structure on a printed circuit board and the top surface of a coin were acquired.

• 한국자동차공학회논문집
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• 제18권5호
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• pp.100-107
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• 2010

This paper gives new conceptual descriptions of drag reduction mechanism owing to rotating wheel and moving ground condition when dealing with automotive aerodynamics. Using Computational Fluid Dynamics (CFD), flow simulation of three dimensional automobile configuration made by Vehicle Modeling Function (VMF) is performed and the influence of wheel arch, wheels, rotating wheel & moving ground condition to the automotive aerodynamic performance is analyzed. Finally, it is shown that rotating wheel & moving ground condition decreases automotive aerodynamic drag owing to the reduction of the induced drag led by the decrease of COANDA flow intensity of the rear trunk flow.

• 한국측량학회지
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• 제11권1호
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• pp.7-18
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• 1993

비지형대상물의 전면해석을 위한 다중지점 사진측량강의 설계에는 촬영점의 기하학적 배치, 영상의 기하학적 조건, 기준점 배치 및 조정의 경중률 등 많은 문제들이 복합적으로 포함되어야 하며, 특히 좁고 긴 구조물의 내부를 측량할 경우에는 특수한 사진측량망을 필요로 한다. 본 연구에서는 구조물 내부의 전면해석에 수반되는 주요 난점들의 해결안을 제시하고 결과의 정확도 및 신뢰도의 향상을 기하고자 하였다. 이를 위해 내부의 형상과 크기에 적합한 다중사진측량망을 구성하고 광속조정법에 의하여 3차원 자료를 취득, 강의 구성요소에 따른 정확도에 미치는 영향을 고찰하였다. 아울러 본 연구에서 개발된 과대오차의 검출연산법은 사진측량 해의 신뢰도 향상에 그 활용이 기대된다.