• Title/Summary/Keyword: Jet Position

검색결과 161건 처리시간 0.025초

천리안 수증기 영상을 이용한 태풍진로의 전향위치 예측 연구 (Study on the Prediction of Turning Point of Typhoon Tracks using COMS Water Vapor Images)

  • 김종석;윤일희
    • 한국지구과학회지
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    • 제35권3호
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    • pp.168-179
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    • 2014
  • 이 연구의 목적은 관측주기가 짧은 천리안 위성의 수증기 영상자료를 활용하여 태풍의 전향위치와 시간까지 예측이 가능하도록 하는데 있다. 즉 수증기의 위성영상의 건조슬롯과 제트류의 남북진동의 관계를 이용하여 태풍진로의 전향위치를 보다 정확히 예측하는 것이다. 제트류는 제트스트리크의 위치와 지균풍 ${\upsilon}$성분의 크기에 따라 움직이는데, 지균풍 ${\upsilon}$ 성분이 남쪽방향으로 강화되면 제트류는 원형 제트로 발달하게 된다. 이때 수증기 영상에서는 건조슬롯이 남쪽으로 확대되고, 굴곡수분밴드(CMB) 거리가 좁혀지기 때문에 태풍이 전향하게 된다. 굴곡수분밴드가 위도 $15^{\circ}$ 이하이면 24시간 내에 태풍이 북 또는 북동으로 전향하게 된다. 결과적으로 태풍진로는 건조슬롯의 위치가 $32^{\circ}N$ 이하이면 $20-23^{\circ}N$이하에서 전향(2007년 1호 태풍 콩레이와 2012년 17호 태풍 즐라왓)하고, 건조슬롯이 $35^{\circ}N$ 이상 일 땐 $27^{\circ}$N에서 전향(2007년 4호 태풍 마니)하는 것으로 분석되었다.

초음속 연소기내부의 측면제트분사에 대한 수치적 연구 (Numerical Study of Slot Injection in Supersonic combustor)

  • 김종록;김재수
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2003년도 제21회 추계학술대회 논문집
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    • pp.108-113
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    • 2003
  • The numerical research has been done for the transverse jet behind a rearward- facing step in turbulent supersonic flow without chemical reaction. The purpose of transverse jet is used to improve mixing of the fuel in the combustor. Two- dimensional unsteady flowfields generated by slot injection into supersonic flow are numerically simulated by the integration of Navier-Stokes equation with two-equation k - $\varepsilon$ turbulence model. Numerical methods are used high-order upwind TVD scheme. Eight cases are computed, comprising slot momentum flux ratios and slot position at downstream of the step. The flow is very similar to the cavity flow, because the jet is like an obstacle. Therefore, the numerical results show the periodic phenomenon.

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Atomize법에 의한 용융소재의 고효율 미세화에 관한 연구(제2보 : 이젝터의 원리를 이용한 액체노즐의 액체공급 및 액막생성 기구와 특성) (A Study on the High-Efficiency Atomisation Molten Materials (PART 2 : A Study on the Mechanism of Liquid Supplying and Film Formation by Applying the Ejector Principle))

  • 오재건;조일영
    • 한국분무공학회지
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    • 제3권2호
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    • pp.14-23
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    • 1998
  • The negative pressure as much as 10's mmHg is demanded at nozzle inside, in case of atomizing the large density molten materials. by conventional air jet nozzle. In this study, suction type fluid nozzle is designed by applying the ejector principle in order to clarify the air flow of nozzle inside, mechanism of liquid suction and liquid film formation. The results of this experimental study areas follows. Suction force of liquid is magnified by using liquid nozzle, and it is able to supply the liquid stable. Negative pressure at nozzle inside is varied by throttle angle of liquid nozzle, position and outer diameter of air jet nozzle, and have a influence on liquid suction quantity and liquid film formation.

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DES를 이용한 초음속 유동내 수직 연료분사 유동의 비정상 3차원 해석 (UNSTEADY THREE-DIMENSIONAL ANALYSIS OF TRANSVERSE FUEL INJECTION INTO A SUPERSONIC CROSSFLOW USING DETACHED EDDY SIMULATION)

  • 원수희;문성영;정인석;최정열
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2008년도 학술대회
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    • pp.97-103
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    • 2008
  • Unsteady three-dimensional flowfields generated by transverse fuel injection into a supersonic mainstream are simulated with a DES turbulence model. Comparisons are made with experimental results in term of the temporal eddy position and eddy formation frequency. The vorticity field around the jet exit is also analyzed to understand the formation mechanism of the jet vortical structures. Results indicate that the DES model correctly predicts the convection characteristics of the large scale eddies. However, it is also observed that the numerical results slightly overpredict the eddy formation frequency. The jet vortical structures are developed from the competing vortices in the recirculation region of upstream boundary.

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DES를 이용한 초음속 유동내 수직 연료분사 유동의 비정상 3차원 해석 (UNSTEADY THREE-DIMENSIONAL ANALYSIS OF TRANSVERSE FUEL INJECTION INTO A SUPERSONIC CROSSFLOW USING DETACHED EDDY SIMULATION)

  • 원수희;문성영;정인석;최정열
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2008년 추계학술대회논문집
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    • pp.97-103
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    • 2008
  • Unsteady three-dimensional flowfields generated by transverse fuel injection into a supersonic mainstream are simulated with a DES turbulence model. Comparisons are made with experimental results in term of the temporal eddy position and eddy formation frequency. The vorticity field around the jet exit is also analyzed to understand the formation mechanism of the jet vortical structures. Results indicate that the DES model correctly predicts the convection characteristics of the large scale eddies. However, it is also observed that the numerical results slightly overpredict the eddy formation frequency. The jet vortical structures are developed from the competing vortices in the recirculation region of upstream boundary.

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고해상 스테레오PTV (High-Resoultion Stereoscopic PTV)

  • 도덕희;이원제;조용범;편용범;장석원
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2002년도 학술대회지
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    • pp.511-512
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    • 2002
  • A new stereoscopic PTV was developed using two CCD cameras, stereoscopic photogrammetry based on a 3D-PTV principle. The arrangement of the two cameras was based on angular position. The calibration of cameras and the pair-matching of the three-dimensional velocity vectors were based on Genetic Algorithm based 3D-PTV technique. The constructed Stereoscopic W technique was tested on the standard images of the impinged jet proposed by VSJ. The results on the turbulent properties of the jet obtained by the constructed system showed a good agreement with the original LES data.

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The monitoring inner jet of 3C84 with GMVA

  • Kim, Min-Joong;Lee, Sang-Sung;Krichbaum, T.P.;Kim, Sung-Eun
    • 천문학회보
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    • 제35권2호
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    • pp.34.2-34.2
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    • 2010
  • The 3C84 (NGC 1275), one of Seyfert 2 galaxy, is an interesting object with its peculiar sub-mas structure. We found that the inner jet (r < 2.5mas) of 3C84 seemed to even changed its position angle and flux over one and a half years based on the result of global 86GHz VLBI survey (Lee et al. 2008). In order to confirm the 'precession' of jet, we observed the object in 4 epochs May07, Oct.07, May08 and Oct.08 with the GMVA (Global mm-VLBI Array) at 3mm (86.25GHz) and the each observation time is about 14 hours. Here we present observation and preliminary result of Oct.07 and May08 epochs.

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Investigation of the shock structural formation of the supersonic nozzle jet with longitudinal variation of coaxial pipe location

  • Roh, Sung-Cheoul;Park, Jun-Young;Kim, Soo-Yong
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2004년도 제22회 춘계학술대회논문집
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    • pp.784-788
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    • 2004
  • A visualization study of shock formation of the supersonic jet nozzle using a Shadowgraph Method (SM) was carried out to investigate the effect of the longitudinal variation of coaxial pipe end tip position inside the supersonic nozzle. The experiment was performed for the Mach number range from 1.1 to 1.2 at nozzle exit. The well known shock cell structure was shown with the pipe end located deep inside the nozzle for the studied Mach number. With the pipe end approaches nozzle exit, it was found that the shock cell structure disappeared and turned into complex formation. In order to understand the mechanism of the shock structural change, computational simulation was carried out using the Navier-Stokes solver, FLUENT. Topological sketch was added with an aid of the visualization and the numerical simulation.

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고해상 스테레오 PTV (High-Definition Stereoscopic PTV)

  • 도덕희;이원제;조용범;편용범
    • 한국가시화정보학회:학술대회논문집
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    • 한국가시화정보학회 2002년도 추계학술대회 논문집
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    • pp.11-14
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    • 2002
  • A new high-definition stereoscopic PTV was constructed using two CCD cameras, stereoscopic photogrammetry based on a 30-PTV principle. The arrangement of the two cameras was based on angular position. The calibration of cameras and the pair-matching of the three-dimensional velocity vectors were based on Genetic Algorithm based 30-PTV technique. The constructed Stereoscopic PTV technique was tested on the standard images of the Impinging jet proposed by VSJ. The results on the turbulent properties of the jet obtained by the constructed system showed a good agreement with the original LES data.

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An Impact Position Control of the Ink Droplet of Inkjet Printer

  • Cho, Young-Wan
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 2005년도 ICCAS
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    • pp.2509-2512
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    • 2005
  • In this paper, a position control scheme of the ink droplet is presented for the high image quality and print speed inkjet printer. The proposed scheme estimates the impact position and compensates it by control of the fire strobe time based on the dynamic equations describing the moving trajectory of the ink droplet. Compared to the conventional fire strobe control which is based on the simple synchronization the fire strobe with the position signal of the inkjet nozzle, the proposed control scheme provides more accurate impact position control during the carrier is moving with accelerated or decelerated speed as well as constant speed. The availability of printing during the acceleration and deceleration states of the carrier moving enables the print speed up and the frame size down which means the cost down.

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