• 대한기계학회:학술대회논문집
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• 대한기계학회 2002년도 학술대회지
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• pp.443-446
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• 2002

Wake downstream of an object in the stratified flow has been of long-standing interest in fluid dynamics because of its similarity to geophysical flow over topographical terrains and more recently, concerns about the wake left behind a body moving through the ocean thermocline. Decades of studies of geophysical flow have unveiled that the flow downstream of obstacles in stratified flow consists of attached wake and strong internal waves, or separated, fluctuating wake and persistent late wakes, all of which depend on the flow conditions. Among unique and interesting characteristics of the stratified flow past obstacles is the generation of coherent vortex structure in the late wake far downstream of the object. Without the density stratification, the flow field downstream becomes undisturbed after relatively fast diminishing of the near wake. However, no matter how small the stratification is, the flow field downstream self-develops coherent vortex structures even after diminishing of the near wake. This paper present a computational approach to simulate the generation mechanism of the coherent vortex and analysis of the vortical structure.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2002년도 학술대회지
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• pp.611-614
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• 2002

Rotating stall in vaneless diffusers of centrifugal compressor occurs in the diffuser wall due to flow separation at large inlet flow angle. For this reason, the critical inlet flow angles are suggested by several researchers. Beyond this critical angle, flow separates in the diffuser, and develops into rotating stall. This paper studied this critical flow angle. Rotating stall is measured through eight fast-response pressure transducers which are equally spaced around the circumference at the inlet and exit of a vaneless diffuser. Experiments are done from 20000rpm to 60000rpm for the diffuser stall. Two-cell structure which rotates at $6{\~}l0{\%}$ of impeller speed is fully developed at $20000{\~}40000rpm$, and three-cell structure which rotates at $7{\~}9{\%}$ of impeller speed is fully developed at $50000{\~}60000rpm$. This paper shows that the critical inlet flow angle is not constant but related with tip speed of impeller. As tip speed increases, so does the critical inlet flow angle.

• 반도체디스플레이기술학회지
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• 제3권3호
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• pp.37-40
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• 2004

This study presents numerical solutions of three-dimensional laminar flow-field formed by photo resist flow in a slit-coater model. We discuss on the governing equations, laminar viscosities and the computational model applied in our numerical calculation and some results. We prove that the structure of tapered-cavity aid to make uniform pressure-field and boundary effect is an important problem to improve coating uniformity. In view of uniformity improvement, it is necessary to study for the structure of cavity and flow path.

• 한국산학기술학회논문지
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• 제15권3호
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• pp.1294-1298
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• 2014

향후 제작 될 솔레노이드 구조의 방향을 제시하고자 실험 및 유동 특성에 대한 비교 분석 연구가 진행 되어졌다. 실험값과 해석값의 비교 분석은 ANSYS CFD와 전자식 측정 기구를 이용하여 수행하였다. 구조의 3D 모델링은 CATIA V5R18을 이용하였으며, 유동구간의 격자 생성은 ICEM CFD 프로그램을 사용하였다. 유동해석 분석은 수치해석 프로그램인 ANSYS CFD를 이용하여 실험값에 대한 검증이 진행되었다. 실험값을 통해 정밀 필터구간에서 나타난 유량은 $0-10{\ell}/min$ 으로 나타났으며 유동해석결과 최대 $0.18{\ell}/min$로 나타났다. 유동 해석 결과와 실험값의 비교분석을 통해 유동환경에 보다 효율적인 솔레노이드 구조를 제시 할 수 있었다.

• 해양환경안전학회지
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• 제12권4호
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• pp.301-306
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• 2006

인공용승구조물 설치해역의 구조물에 의한 유동분포를 파악하기 위하여 ADCP(Acoustic Doppler Current Profiler)를 이용한 정선관측을 2006년 5월 4일(소조기) 및 5월 30일(대조기)에 실시하였다. 동서-남북(un-component) 유동성분의 분석결과, 조시에 따른 흐름이 전반적으로 남동류가 우세하게 나타났으며 구조물 주변역의 표층에서 수심 $30\sim40m$까지의 유동과 이심에서의 유동이 서로 다르게 나타났다. 연직유동성분(w-component)은 소조기시 구조물 주변해역과 서쪽역에서는 상승류의 흐름이 나타났고 남쪽역, 북쪽역 및 동쪽역에서는 하강류의 흐름이 나타났다. 대조기 W-W line의 낙조시에는 동쪽과 서쪽해역에서 상승류의 흐름이 나타났으며 구조물 중심 동쪽 부근에서 상승류의 흐름이 나타났고 구조물에서 멀어질수록 하강류의 흐름이 나타났다. 대조기시의 분포는 창조시 S-N line에서 상승류의 분포가 전반적으로 나타났다. 또한 구조물 구축 주번해역에서의 단위면적당 상승류의 유량은 대 소조기 창 낙조시에 하강류에 대한 유량보다 크게 나타났다. 소조기에는 창조시보다 낙조시에 더 강하였으며, 대조기에는 창조시가 낙조시보다 큰 유량을 나타내고 있다.

• 대한전기학회:학술대회논문집
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• 대한전기학회 1987년도 전기.전자공학 학술대회 논문집(II)
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• pp.1125-1128
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• 1987

This paper proposes a method which distributes the structure data represented by a tree and handles it. To distribute and handle the structure data, this method partitions a structure data and distributes the partitioned structure in multiple processing element and allocates the partitioned structure. Each processing element includes the structure memory to store the partitioned structure and the structure controller to handle efficiently the distributed structure. As the structure is distributed and is stored in the structure memory and is handled by the structure controller, the processing time is reduced.

• 대한조선학회논문집
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• 제40권5호
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• pp.53-59
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• 2003

Ocean space utilization using VLFS(Very Large Floating Structures) can provide environmental impact free space by allowing sea water flow freely through the floating structure. Use of Pontoon type VLFS for that purpose needs employment of breakwaters for reduction of wave effects. Therefore, in order to maximize advantage of environmental impact free structure, the breakwater should be the one that can allow water flow freely through it, too. In this paper hydroelastic response of a pontoon type structure is analyzed considering breakwaters which allow water flow through its opening at bottom of the breakwaters. Mode superposition technique is used for solving equation of flexible body while interactions between the pontoon and breakwaters is considered based on generalized mode concept. Bi-quadratic nine node higher-order boundary element method is adopted for more accurate numerical treatment near sharp edged body shape. Performance of various combinations of breakwaters is investigated.

• 유체기계공업학회:학술대회논문집
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• 유체기계공업학회 2005년도 연구개발 발표회 논문집
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• pp.819-824
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• 2005

Recently, micro hydropower attracts attention because of its clean, renewable and abundant energy resources to develop. However, suitable turbine type is not normalized yet in the range of micro hydropower and it is necessary to study for the effective turbine type. Moreover, relatively high manufacturing cost by the complex structure of the turbine is the highest barrier for developing the micro hydropower turbine. Therefore, a cross-flow turbine is proposed for micro-hydropower in this study because of its simple structure and high possibility of applying to low head. The purpose of this study is to further simplify the turbine structure and improve the performance, A guide vane is removed and the runner chamber is made compact using a new air supply method. The results show that the efficiency of the turbine is improved in a wide operating range and the size of the turbine is remarkably reduced.

• 한국자동차공학회논문집
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• 제12권6호
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• pp.74-79
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• 2004

The effects of change in injection pressure on spray structure have been investigated in high temperature and pressure field. To analyze the structure of evaporative diesel spray is important in speculation of mixture formation process. Also emissions of diesel engines can be controlled by the analyzed results. Therefore, this study examines the evaporating spray structure by using a constant volume vessel. The injection pressure is selected as the experimental parameter, is changed from 72 MPa to 112 MPa with a high pressure injection system(ECD-U2). The PIV(Particle Image Velocimetry) technique was used to capture flow variation of the evaporative diesel spray. A study on the mixture formation process of diesel spray was executed by the results of flow analysis in this study. Consequentially the large-scale vortex flow could be found in downstream spray and the formed vortex governs the mixture formation process in diesel spray.

• 대한기계학회논문집A
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• 제33권6호
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• pp.573-576
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• 2009

We present a passive flow-rate regulator, capable to compensate inlet pressure variation and to maintain a constant flow-rate for precise liquid control. Deflection of the parallel membrane valves in the passive flowrate regulator adjusts fluidic resistance according to inlet fluid pressure without any external energy. Compared to previous passive flow-rate regulators, the present device achieves precision flow regulation functions at the lower threshold compensation pressure of 20kPa with the simpler structure. In the experimental study, the fabricated device achieves the constant flow-rate of $6.09{\pm}0.32{\mu}l/s$ over the inlet pressure range of $20{\sim}50$ kPa. The present flow-rate regulator having simple structure and lower compensation pressure level demonstrates potentials for use in integrated micropump systems.