• 대한의용생체공학회:의공학회지
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• 제17권4호
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• pp.515-524
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• 1996

The flow characteristics of developing unsteady laminar flow in a square-sectional $180^{\circ}$ curved duct are experimentally investigated by using laser doppler velocimerty (LDV) system with data acquisition and processing system of rotating machinery resolver(RMR) and PHASE software. The major flow characteristics of developing laminar pulsating flows are presented by mean velocity profilel velocity distribution of secondary flow, wall shear stress distributions, entrance lengths according to dimensionless angular frequency($\omega^+$), velocity amplitude ratio($A^1$), and time-averaged Dean number($De_ta$). The velocity profiles and wall shear stress distribution of laminar pulsating flow with dimensionlessangular frequency show the flow characteristics of the quasi-steady laminar flow in a curved duct. The developing region of laminar pulsatile flows in a square-sectional $180^{\circ}$ curved duct is extended to the curved duct angle of approximately $120^{\circ}$ under the present experimental condition.

• 대한기계학회논문집B
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• 제29권5호
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• pp.545-553
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• 2005

In the present study, The characteristics of developing steady laminar flows of a straight duct connected to a $180^{\circ}$ curved duct were examined In the entrance region through experimental measurement. Flow characteristics such as shear stress distributions, pressure distributions and friction coefficient experimentally in a square cross-sectional straight duct by using the PIV system. For the PIV measurement by particles produced from mosquito coils particles. The experimental data were obtained at 9 points dividing the test sections by 400mm. Experimental results can be summarized as follows. Critical Reynolds number, $Re_{cr}$ which indicates transition from laminar steady flow to transition steady flow was 2,150. Shear stress per unit length on the wall was stronger than that in the fully developed flow region. This was attributed to the fact that shear stress and pressure loss in the curvature of a duct were increased. Pressure distributions were gradually decreased irrespective of Reynolds number In the whole test section. This trends were in a good agreement with the reference results. Pipe friction coefficient in the steady state flow region was calculate from method of least squares. The co-relationship between fiction coefficient and Reynolds number was established as follow; ${\lambda}=56/Re$.

• 농촌계획
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• 제21권2호
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• pp.177-188
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• 2015

This research was establishment of landscape formation plan to Yusang village region Yeongcheon city. Literature research, field research, surveys carried out for this purpose. In addition, by utilizing design code that appears in the common characteristics of the rural scenic views of the region in improving the quality of life of the local population and preserve the indigenous landscape as well as improve the quality of rural landscapes, management, capital town of the region to form Yeongcheon the center was established in the landscape plan form. The natural environment of the capital region for the landscape formation plan, Humanities and Social Environment, Landscape Resources Status, Social Consciousness, landscape map, landscape design, code identification and basic design and planning through the basic steps to derive design guidelines were applied to the landscape formation plan. Formation landscape plan for the regional launch of the regional landscape improvements, region entrance space and yusang reservoirs place, rest zone in the sacred tree and nurse trees around the plan, and repair the town hall. residents living village road maintenance to improve the environment, and develop a detailed plan, such as the lungs maintenance. The plan is likely to be able to contribute to improving the quality of life of the people and landscapes to improve regional, creating a guide for future business landscape is formed to have a significant advantage as a basis.

• 한국컴퓨터정보학회논문지
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• 제13권6호
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• pp.243-251
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• 2008

본 논문에서는 지문 인식에 효율적으로 적용 가능하도록 출입 보안을 위한 레이블링을 이용한 영역 분리 및 지문 중심점 추출 알고리즘을 제안한다. 출입 보안 기술은 출입통제, 근태관리, 컴퓨터 보안, 전자상거래 인증, 정보보호 등이 있다. $128{\times}128$ 크기의 원 영상을 $4{\times}4$ 픽셀 크기로 나누어 방향 영상을 추출하고 잘못된 방향 영상에 대하여 방향 평활화 작업을 수행한다. 추출된 방향 평활화 영상을 각 방향별로 레이블링을 이용하여 영역을 분리하고 3가지 이상의 방향 변화가 나타나는 블록을 중심점으로 추출한다. 기존 방법에서 사용한 중심점 가능 영역이나 중심점 후보 영역을 탐색하지 않고 최대 방향과 레이블링을 이용한 방향별 영역 분리를 통하여 중심점을 추출함으로써 인식률과 매칭률을 높이고자 한다. 실험에 사용된 300개의 지문에 대하여 실험한 결과, Poincare 지수 방법은 94.05%의 추출율을 보였고 제안한 방법은 97.11%의 추출율을 보였다.

• 한국방사선학회논문지
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• 제13권2호
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• pp.175-183
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• 2019

뇌신경계 인터벤션 시술은 장시간의 시술로 인해 피부의 수포, 탈모, 홍반 등의 방사선 피폭으로 인한 위해가 빈번히 보고되고 있다. 인체공학적으로 제작된 Bismuth (원자번호 83;Bi) 차폐체를 뇌혈관계 인터벤션 시술에 적용함으로써 의료방사선 피폭으로부터 두피 및 수정체의 방사선 피폭을 최소화하고자 하였다. 측정 부위는 4부위로 후두부(9 points), 양쪽 측두부(12 points), 양쪽 수정체부(6 points), 코 끝부(6 points)이며, 측정 소자는 광자극 형광 선량계(Optically Stimulated Luminescence Dosimeter: OSLD)를 각 지점(points)에 측정기를 부착 후 자체 제작된 Bismuth차폐 기구를 사용 전(A그룹)과 후(B그룹)를 측정한 후 피부표면선량(entrance surface dose)을 비교 분석하였다. A 그룹(Bismuth unshield)과 B 그룹(Bismuth shield)의 피부선량 평균은 A 그룹은 92.44 mGy였고, B 그룹은 67.55 mGy로 측정되었다. A 그룹에 비해 B 그룹에서 평균 26.92% 감소되었다. 후두부의 피부선량 평균은 A 그룹(9 point)은 146.08 mGy, B 그룹(9 point)은 103.23 mGy로 측정되었고 A 그룹에 비해 B 그룹에서 평균 29.32 % 감소하였다. 측두부의 피부선량 평균은 A 그룹(6 point)은 101.90 mGy, B 그룹(6 point)은 72.69 mGy로 측정되었고 A 그룹에 비해 B 그룹에서 평균 28.67% 감소하였다. 수정체부의 피부선량 평균은 A 그룹(3 point)은 27.51 mGy, B 그룹(3 point)은 21.39 mGy로 측정되었고 A 그룹에 비해 B 그룹에서 평균 22.26% 감소하였다. Bismuth 차폐체의 사용은 뇌혈관 중재적 시술 후 나타날 수 있는 일시적 탈모 및 기타 확률적 영향에 따른 방사선 장해를 감소시킬 수 있는 대안이 될 것으로 사료된다.

• 한국자동차공학회논문집
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• 제9권1호
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• pp.102-111
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• 2001

To describe the air flow characteristics within an air cleaner cover and mass air flow sensor (MAFS) entry region installed in a 3.0L engine air induction system, flow visualization, velocity and turbulence intensity measurements were taken in several view planes. A detailed knowledge of the interaction between the design parameters and the flow structures will enhance our understanding of the motions within the flow field and enable engineers to optimize the induction system and reduce the signal-to-noise ratio in the MAFS output. Emphasis is placed on the analysis of coherent motions and the controlling parameters which affect the air flow in the MAFS entrance region over a flow rate of 13-240 kg/hr. The high speed motion pictures illustrated that the air flow generated within the air cleaner cover under steady state condition is quite complex. In both axial and radial planes of the main passage it was found that the flow pattern is remarkably influenced by the air cleaner cover and main passage configuration. A comparison of the flow patterns and measurements in the original and modified air cleaner cover is presented. Measurements from the MAFS indicated an significant reduction in pressure drop and signal noise for the modified cover as compared with the original cover, over an air flow rate of 13-240 kg/hr.

• 대한기계학회논문집B
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• 제29권10호
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• pp.1092-1100
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• 2005

In the present study, characteristics of steady state laminar flows of a straight duct connected to a 180$^{o}$ curved duct were examined in the entrance region through experimental and numerical analyses. For the analysis, the governing equations of laminar flows in the Cartesian coordinate system were applied. Flow characteristics such as velocity profiles and secondary flows were investigated numerically and experimentally in a square cross-sectional straight duct by the PIV system and a CFD code(STAR CD). For the PIV measurement, smoke particles produced from mosquito coils. The experimental data were obtained at 9 points dividing the test sections by 400 3m. Experimental and numerical results can be summarized as follows. 1) Reynolds number, Re was increased, dimensionless velocity profiles at the outer wall were increased due to the effect of the centrifugal force and secondary flows. 2) The intensity of a secondary flow became stronger at the inner wall rather than the outer wall regardless of Reynolds number. Especially, fluid dynamic phenomenon called conner impact were observed at dimensionless axial position, x/D$_{h}$=50.

• Tribology and Lubricants
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• 제14권1호
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• pp.7-13
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• 1998

The static characteristics of a five-pad tilting pad journal bearing of load on pad (LOP) type have been investigated experimentally under the different values of bearing load and shaft speed. The diameter and length of the bearing are 300.91 mrn and 149.8 mm, reslx;ctively. Circumferential distribution of the film pressure, film thickness, journal surface temperature and beating surface temperature are measured. A noticeable inlet pressure rise is observed at the entrance of each pad, especially the bottom pad. The inlet pressure is increased by the increase of shaft speed as well as bearing load. In the five-pad tilting pad joumal bearing of LOP type, almost all of beating load is being carried only by the bottom pad. The maximum bearing surface temperature is observed at near the minimum film thickness. It is observed that the metal temperature of the mid-plane is higher than that of the edge at the inlet region, while the metal temperature of the edge is higher than that of the mid-plane at the outlet region.

• 대한기계학회논문집B
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• 제23권2호
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• pp.243-253
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• 1999

The dual reciprocity boundary element method (DRBEM) is used to solve the Graetz problem of laminar flow inside circular duct. In this method the domain integral tenn of boundary integral equation resulting from source term of governing equation is transformed into equivalent boundary-only integrals by using the radial basis interpolation function, and therefore complicate domain discretization procedure Is completely removed. Velocity profile is obtained by solving the momentum equation first and then, using this velocities as Input data, energy equation Is solved to get the temperature profile by advancing from duct entrance through the axial direction marching scheme. DRBEM solution is tested for the uniform temperature and heat flux boundary condition cases. Local Nusselt number, mixed mean temperature and temperature profile inside duct at each dimensionless axial location are obtained and compared with exact solutions for the accuracy test Solutions arc in good agreement at the entry region as well as fully developed region of circular duct, and their accuracy are verified from error analysis.

• Journal of Mechanical Science and Technology
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• 제17권12호
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• pp.2027-2033
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• 2003

The purpose of this study is to investigate the stratification of fuel vapor with different in-cylinder flow, piston cavity and injection timings in an optically accessible engine. Three different piston shapes that are F(Flat), B(Bowl) and R(Re-entrance) types were used. The images of liquid and vapor fuel were captured under the motoring condition using Laser Induced Exciplex Fluorescence technique. As a result, at early injection timing of 270 BTDC, liquid fuel was evaporated faster by tumble flow than swirl flow, where most of fuel vapor were transported by tumble flow to the lower region and both sides of cylinder for the F-type piston. At late injection timing of 90 BTDC, tumble flow appears to be moving the fuel vapor to the intake side of the cylinder, while swirl flow convects the fuel vapor to the exhaust side. The concentration of mixture in the center region was highest in the B-type piston, while fuel vapor was transported to the exhaust side by swirl flow in F and R-type pistons. At the injection timing of 60 BTDC, the R-type piston was better for stratification due to a relatively smaller bowl diameter than the others.