• 제목/요약/키워드: Multi-Jet

검색결과 182건 처리시간 0.029초

평면벽면분류의 유입경계조건을 가지는 개수로 유동에 관한 수치적 연구 (A Numerical Study on the Open Channel Flow with Plane Wall Jet Inlet Boundary Condition)

  • 설광원;이상룡
    • 대한기계학회논문집
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    • 제13권2호
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    • pp.287-298
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    • 1989
  • 본 수치적 해석에서는 H$_{w}$/H$_{g}$의 비가 5.0~16.7의 범위에서 수행된 실험결과를 바탕으로 기존의 k-.epsilon. 난류모델을 사용하여, 고려하고자 하는 변수, 즉 유입유속, 입구 게이트의 높이, 수위, 배플의 유.무등에 따라서 액체의 유동형태가 어떻게 변하는가를 살펴 보고자 한다.다.

평면벽면분류의 유입경계조건을 가지는 개수로 유동 및 배플의 영향에 관한 실험적 연구 (An experimental study on the open channel flow with plane wall jet inlet boundary condition and effects of a baffle)

  • 방병렬;설광원;이상용
    • 대한기계학회논문집
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    • 제12권6호
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    • pp.1399-1406
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    • 1988
  • 본 연구에서는 수로의 폭이 작고(W=74mm) H$_{w}$/H$_{g}$가 5.0~16.7의 범 위인 경우에 레이져 유속계를 이용하여 주어진 유동조건, 예컨대, 유입유속, 입구게이 크(gate)의 높이, 수위, 배플의 유. 무및 높이, 그리고 배플의 위치등에 따라서 액체 속도의 분포가 어떻게 변화하는가를 정성적으로 관찰해 보고자 하는데 주안점을 두었 다. 본 실험 결과는 차후에 계속될 후래시 증발현상에 관한 실험및 해석적 접근에 관한 기초 자료로서 활용하는데에도 그 목적이 있다.다.

석판재용 물다듬 패턴무늬 가공 전용기 개발 (Development of water cropping machine for slab pattern processing)

  • 김경철;고민혁;김종태;이지수;유범상
    • 한국산학기술학회논문지
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    • 제14권9호
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    • pp.4130-4135
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    • 2013
  • 본 논문은 석재의 표면 마감 시 다양한 패턴의 무늬를 가공하기 위한 전용기에 대한 연구이다. 기존의 평범한 무늬에 대하여 기능 및 예술성을 부여하여 석판의 활용 범위를 확대 발전시키고자 한다. 이에 본 연구에서는 Water-Jet을 이용하여 석재의 표면 가공 시 다양한 패턴에 대한 적용이 가능한 전용기를 개발하였다. 전용기는 석판을 이송하는 이송 기구, 다양한 패턴 무늬 생성을 위한 노즐 이송 기구, 초고압수를 이용한 멀티노즐 기구, 모션 제어를 위한 제어시스템, 그리고 패턴 무늬 선택을 위한 S/W로 구성되어 있다. 개발되어진 전용기에 대한 다양한 패턴 무늬에 대한 실험을 통하여 성능 평가를 하였다. 이를 통하여 다양한 종류의 패턴 무늬 가공이 가능하며, 가공 오차 ${\pm}0.5mm$의 정밀도를 갖는 전용기를 개발하였다.

다중 홉 광 버스트 교환망에서 종단간 수율 향상을 위한 홉 단위 우선 순위 증가 기법 (Hop-by-Hop Priority Increasing Scheme for Improving End-to-end Throughput in Multi-Hop OBS Networks)

  • 김병철;조유제
    • 대한전자공학회논문지TC
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    • 제40권10호
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    • pp.35-42
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    • 2003
  • 본 논문에서는 광 버스트 교환 방식에서 사용되는 제어 패킷 처리 시간 보상 기법 및 자원 예약 기법을 분류하고 다중 홉 환경에서 대표적인 예약 방식인 OT/DR (Offset Time/Delayed Reservation) 기반 JET(Just-Enough-Time) 방식의 문제점인 Path length priority effect를 분석하였다. 그리고, 이러한 문제점을 해결하면서 입력 FDL(Fiber Delay Line)을 사용하여 홉 단위로 우선 순위를 증가시켜 종단간 수율을 개선시킬 수 있는 FDL/DR 방식 기반의 홉 단위 우선 순위 증가 기법을 제안하고 시뮬레이션을 통하여 성능을 비교 분석하였다. 시뮬레이션을 통한 성능 분석 결과 제안된 방식은 다중 홉 환경에서 path length priority effect로 인해 발생하는 기존 방식의 문제점을 개선하여 종단간 성능이 향상됨을 알 수 있었다.

Novel Development of Electrowetting Display

  • Cheng, W.Y.;Chang, Y.P.;Lo, K.L.;Lee, D.W.;Lee, H.H.;Kuo, S.W.;Hsiao, C.C.;Chen, K.T.;Tsai, Y.H.;Chen, Y.C.;Fuh, S.Y.;Wang, C.W.;Su, P.J.;Chiu, W.W.;Lee, K.C.;Shiu, J.W.
    • 한국정보디스플레이학회:학술대회논문집
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    • 한국정보디스플레이학회 2008년도 International Meeting on Information Display
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    • pp.1240-1243
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    • 2008
  • The 6- inch electrowetting display (EWD) can be successfully developed by ink jet printing (IJP) technique. Due to the drop-on-demand characteristic of IJP technology, colored oil can be precisely dosed into the unit pixel. Here, we present the active matrix EWD in this article. By adopting this technique to dose different colored oils, single layer Multi-color EWD without adopting color filter can be achieved in the future.

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점착 유층과 계면활성제 액적의 충돌에 의한 에멀젼 형성 (Generation of emulsions due to the impact of surfactant-laden droplet on a viscous oil layer on water)

  • 이동훈;김도형;김일두;이진기
    • 한국가시화정보학회지
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    • 제20권3호
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    • pp.10-18
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    • 2022
  • We present an experimental investigation on emulsions created during the impact process between a surfactant-laden droplet and an oil layer on water. By varying the surfactant concentration and the viscosity of oil layer, we created emulsions and visualized them using multi-dimensional high-speed imaging. Our analysis shows that the emulsions are more likely to be unstable and decay within a minute if the impacting droplet contains more surfactant. We also found that there are three mechanisms of generation of emulsions depending on the concentration of surfactant and the viscosity of oil layer; the jet pinch-off, cavity pinch-off, and tearing of oil layer. Jet and cavity pinch-off turned out to be dominant mechanisms for high oil viscosities, while tearing of oil layer is dominant for low oil viscosities. Our result is potentially useful in designing optimal dispersant properties for offshore oil contamination.

KaVA and EAVN large program on two Supermassive Black Holes, Sgr A∗ and M87

  • Sohn, Bong Won;Kino, Motoki
    • 천문학회보
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    • 제44권2호
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    • pp.52.1-52.1
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    • 2019
  • Exploring the vicinity of super-massive black holes (SMBHs) is one of the frontiers in astrophysics. KaVA AGN Science WG has launched its Large Program in 2014 focusing on two SMBHs, Sgr A∗ and M87. They are selected based on their large apparent size. Sgr A∗ is the excellent laboratory for studying gas accretion process onto SMBH and M87 is well known as the best case for investigating plasma outflow ultimately driven by SMBH. For Sgr A∗, KaVA and EAVN provides superb UV-coverage on its emitting region and its scattering medium. In the case of M87, we have conducted high cadence dual-frequency (22and 43GHz )VLBI monitoring to clarify the global profile of the M87 jet velocity field and the spectral index map, which should reflect global structure of magnetic fields in the jet. From 2017, the AGN LP is recognized as multi-wavelength EHT project, conducting quasi-simultaneous coherent observations of M87 and Sgr A∗ with the Event Horizon Telescope (EHT) during its campaign observation periods. AGN WG is reviewing and revising its LP to convert it to EAVN LP. We will briefly report our scientific results and future plan which includes even broader international collaboration, namely East-Asia to Italy Nearly Global (EATING) VLBI to reach higher angular resolution.

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스테레오 PIV 기법에 의한 임펠러 와류유동의 3차원 구조측정 (Identification on the Three-Dimensional Vortical Structures of Impeller Flow by a Multi-Plane Stereoscopic PIV Method)

  • 윤상열;김경천
    • 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.

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MEASURING THE CORE SHIFT EFFECT IN AGN JETS WITH THE EXTENDED KOREAN VLBI NETWORK

  • JUNG, TAEHYUN;DODSON, RICHARD;HAN, SEOG-TAE;RIOJA, MARIA J.;BYUN, DO-YOUNG;HONMA, MAREKI;STEVENS, JAMIE;VICENTE, PABLO DE;SOHN, BONG WON
    • 천문학회지
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    • 제48권5호
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    • pp.277-284
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    • 2015
  • We present our efforts for extending the simultaneous multi-frequency receiver system of the Korean Very Long Baseline Interferometry (VLBI) Network (KVN) to global baselines in order to measure the frequency-dependent position shifts in Active Galactic Nuclei (AGN) jets, the so called core shift effect, with an unprecedented accuracy (a few micro-arcseconds). Millimeter VLBI observations with simultaneous multi-frequency receiver systems, like those of the KVN, enable us to explore the innermost regions of AGN and high precision astrometry. Such a system is capable of locating the frequency dependent opacity changes accurately. We have conducted the feasibility test-observations with the interested partners by implementing the KVN-compatible systems. Here we describe the science case for measuring the core shift effect in the AGN jet and report progress and future plans on extending the simultaneous multi-frequency system to global baselines.

스테레오 PIV 기법에 의한 임펠러 와류유동의 3차원 구조측정 (Identification on the Three-Dimensional Vortical Structures of Impeller Flow by a Multi-Plane Stereoscopic PIV Method)

  • 윤상열;김경천
    • 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.