• 제목/요약/키워드: Jet core

검색결과 148건 처리시간 0.03초

하나로 원형 조사공의 안내관 제트유동 억제에 대한 해석 (THE ANALYTIC ANALYSIS OF SUPPRESSING JET FLOW AT GUIDE TUBE OF CIRCULAR IRRADIATION HOLE IN HANARO)

  • 박용철;우상익
    • 한국전산유체공학회지
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    • 제10권2호
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    • pp.1-6
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    • 2005
  • The HANARO, a multi-purpose research reactor of 30 MWth, open-tank-in-pool type, has been under normal operation since its initial criticality in February, 1995. The HANARO is composed af inlet plenum, grid plate, core channel with flow tubes and chimney. The reactor core channel is located at about twelve meters (12 m) depth of the reactor pool and cooled by the upward flow that the coolant enters the lower inlet of the plenum, rises up through the grid plate and the core channel and comes out from the outlet of chimney. A fission moly guide tube is extended from the reactor core to the top of the reactor chimney for easily loading a fission moly target under the reactor normal operation. But active coolant through the core can be quickly raised up to the top of the chimney through the guide tube by jet flow. This paper describes an analytical analysis that is the study of the flow behavior through the guide tube under reactor normal operation and unloading the target. As results, it was conformed through the analysis results that the flow rate, reduced to about fourteen kilogram per second (14 kg/s) from the original flow rate of sixteen point three kilogram per second (16.3 kg/s) did not show the guide tube jet.

극저온 제트 유동에 대한 분사기 형상의 영향 (Effect of Injector Geometry on Cryogenic Jet Flow)

  • 조성호;박구정;길태옥;윤영빈
    • 한국항공우주학회지
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    • 제39권4호
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    • pp.348-353
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    • 2011
  • 액체 질소를 이용하여 극저온 단일 제트 유동의 특성을 관찰하였다. 고압 챔버 내부에 액체 질소를 분사하여 단일 제트를 생성, 주위기체압력을 변화시킴으로써 아임계 조건부터 초임계 조건의 주위 환경에 따른 제트의 특성 변화를 확인하였다. 또한 분사기의 길이 대 직경비 및 분사기 내부 형상의 변화에 따른 제트의 특성 변화를 파악하였다. 유동 가시화를 통하여 극저온 제트의 형상 및 액주의 지름을 측정하였으며, 이로부터 액주의 확산각을 계산하여 이전 연구 결과와 비교하였다. 아임계 조건 및 초임계 조건에서의 제트의 형상 변화를 관찰하였으며, 주위기체압력이 대기압과 동일할 경우 제트 유동에서 불안정이 발생함을 확인하였다. 또한 주위기체압력이 증가함에 따라 액주의 확산각이 점차 증가하다가 일정 압력 이상에서 거의 일정하게 유지됨을 확인하였다.

원형분사제트 조절을 통한 유동특성 및 제트 벡터링의 효과 고찰 (Experimental Studies on Flow Characteristics and Thrust Vectoring of Controlled Axisymmetric Jets)

  • 조형희;이창호;이영석
    • 한국추진공학회지
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    • 제1권1호
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    • pp.33-45
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    • 1997
  • 자유제트를 제어하는 방법중 하나는 분사제트 주위에 형성되는 와류를 조절하는 것이다. 이를 위하여 제트노즐 주위에 환형관을 설치하여 환형관으로부터 2차제트를 분사 또는 흡입함으로써 제트주위에 형성되는 전단류를 변화시켰다. 2차제트를 분사하는 경우(R<1.0) 주제트 주위에 형성되는 와류의 발달을 억제함으로써 제트포텐셜코어의 길이가 아주 길어지는 제트유동을 얻을 수 있었고 흡입하는 경우에는(R>1.0) 제트주위의 전단류가 흡입비 R=1.3~l.65에서 대류불안정성에서 절대불안정성으로 바뀜으로써 형성된 와류가 하류에서 제트중심부까지 발전, 결합되는 것을 방지하여 더 긴 포텐셜코어와 중심에서 낮은 난류강도를 얻었다. 위의 결과는 환형관 주위에 부착한 깃의 높이 변화에 따라서 변화하였는데, 이것은 깃이 환형관을 통한 흡입유동의 유로역할을 함으로써 출구 주위의 유체가 직접흡입되는 것을 방지하기 때문이다. 분사제트 벡터링을 위하여 제트노즐 주위의 환형관을 이등분하여 한쪽으로만 흡입함으로써 제트주위에 다른 전단류를 형성함과 동시에 코안다(Goanda)효과를 이용하여 분사제트를 편향시켰다. 편향되는 정도 및 난류성분은 흡입속도비에 따라서 크게 바뀌었다. 실험은 속도분포와 난류강도 측정이 수행되었으며 가시화를 이용하여 유동특성을 관찰하였다.

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평면제트와 충돌면과의 거리변화에 따른 열전달 특성 (Heat Transfer characteristics of distance between impinging surface and a plane jet)

  • 김동건
    • Journal of Advanced Marine Engineering and Technology
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    • 제22권5호
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    • pp.588-594
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    • 1998
  • Heat transfer characteristics of distance between impinging surface and a plane jet were experi-mentally investigated. The local heat transfer coefficients were measured by a thermochromic liq-uid crystal(TLC) The jet Reynolds number studied was varied over the range from 10,000310 to 30,000310 the nozzle-to-plate distance (H/B) from 4 to 10. It was observed that the Nusselt number increases with Reynolds number the occurrence of the secondary peak in the Nusselt number is within the potential core region the potential core of the jet flow can reach the impinging surface so that the wall jet can a transition from laminar to turbulent flow resulting in a sudden increase in the heat transfer rate.

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원형제트출구 전단류 조절에 따른 제트충돌면에서의 열전달 특성 ( 2 ) - 음향여기된 제트 - (Heat Transfer Characteristics on Impingement Surface with Control of Axisymmetric Jet ( 2 ) - With Acoustic Excitation -)

  • 황상동;이창호;조형희
    • 대한기계학회논문집B
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    • 제24권3호
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    • pp.373-381
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    • 2000
  • The flow and heat transfer characteristics on the impingement surface can be controlled by the change of vortex with the acoustic excitation, because the flow characteristics of an impinging jet are affected strongly by the vortices formed at the jet exit. To investigate the effects of acoustic excitation, we measured the velocity, turbulent intensity distributions for the free jet and local heat transfer coefficients on a impingement surface. As the acoustic excitation, subharmonic frequency of excited frequency plays an important role to the control of the jet flow. If the vortex pairings are promoted by the acoustic excitation, turbulence intensity of the jet flow is increased quickly. On the other hand if the vortex pairings are suppressed, the jet flow has low turbulence intensity at the center of the jet. Therefore, the low heat transfer rates are obtained on the impingement plate for a small nozzle-to-plate distance. However, it has high heat transfer rates at a large distance between the nozzle and plate due to the increasing of potential-core length.

헬륨 기체분류의 정상적 비정상적 거동에 관한 연구 (A Study on Steady and Unsteady Behavior of Helium Jet in the Stationary Atmosphere)

  • 김봉곤;서용권;하종률;권순석
    • 한국자동차공학회논문집
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    • 제1권3호
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    • pp.34-45
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    • 1993
  • This study aims to analyze the mixing characteristics of hydrogen considered as a new fuel for internal combustion engines. As the physical property of helium gas is similar to that of hydrogen, helium gas was used in this study. To analyze the steady and unsteady behavior of jet, helium gas was injected into the stationary atmosphere at the normal temperature and pressure. Concentration of helium gas in the center of jet flow is in inverse proportion with axial distance from the nozzle tip. This agrees with the free jet theory of Schlichting. The relative equation for dimensionless concentration to radial/axial distance the axial distance of potential core region, the cone angle a of the jet flow and the relative equation for arriving distance of the front of jet flow to the lapse of time are obtained. But free jet theory of Schlichting in the dimensionless concentration is not in agreement with the present experimental results of the distance of the radial direction. It needs more study. When the arrival frequency of jet flow is used as a parameter, the transition area changing from unsteady flow area into steady flow area becomes gradually wider downstream, but its ratio for the whole unsteady flow area gradually decreases.

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정현파 형상 노즐 제트의 유동특성에 관한 실험적 연구 (Experimental Study on the Flow Characteristics of Sinusoidal Nozzle Jet)

  • 김학림;;이상준
    • 한국가시화정보학회지
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    • 제7권2호
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    • pp.28-34
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    • 2010
  • Two turbulent jet with different sinusoidal nozzle exit configurations of in-phase and $180^{\circ}$ out-of-phase were investigated experimentally using a smoke-wire method and a hot-wire anemometry. Mean velocity and turbulence intensity were measured at several downstream locations under $Re_D\;=\;5000$. For the case of in-phase nozzle configuration, the length of potential core exhibits negligible difference with respect to the transverse locations (0, $\lambda/4$ and $\lambda/2$), similar to that of a plane jet. On the other hand, a maximum difference of 30% in the potential-core length occurs for the $180^{\circ}$ out-of-phase configuration. The spatial distributions of turbulence intensities also show significant difference for the nozzle of $180^{\circ}$ out-of-phase, whereas non-symmetric distribution is observed in the near-exit region(x/D = 1) for the in-phase sinusoidal nozzle jet. Compared to a slit planc jet, the sinusoidal nozzle jets seem to suppress the velocity deficit as the flow goes downstream. The sinusoidal nozzle jet was found to decrease turbulent intensity dramatically. The flow visualization results show that the flow characteristics of the sinusoidal nozzle jet are quite different from those of the slit plane jet.

Fission Moly 표적을 장전하기 위한 안내관의 제트유동 억제 후 하나로 노심 유량분포 (FLOW DISTRIBUTION IN THE CORE OF HANARO AFTER SUPPRESSING THE JET FLOW IN THE GUIDE TUBE USED FOR LOADING FISSION MOLY TARGET)

  • 박용철;이병철;김봉수;김경련
    • 한국전산유체공학회지
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    • 제10권4호통권31호
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    • pp.66-71
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    • 2005
  • HANARO, a multi-purpose research reactor, 30 MWth open-tank-in-pool type, is planning to produce a fission moly-99 of radio isotopes, a mother nuclide of Tc-99m, a medical isotope and a target handling tool is under development for loading and unloading it in a circular flow tube (OR-5) of HANARO. A guide tube is extended from the reactor core to the top of the reactor chimney for easily loading the target under a normal operation of the reactor. But active coolant through the core can be quickly raised up to the top of the chimney through the guide tube. The jet flow was suppressed in the guide tube after reducing the inner diameter of a flow restriction orifice installed in the OR-5 flow tube for adding the pressure difference in the flow tube. This paper describes an analytical analysis to calculate the flow distribution in the core of HANARO after suppressing the jet flow of the guide tube. As results, it was confirmed through the analysis results that the flow distribution in the core of HANARO were not adversely affected.

하나로 원형 조사공의 안내관 유동특성 (Flow Characteristics for Guide Tube of Circular Irradiation Hole in HANARO)

  • 박용철;우종섭
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2004년도 춘계학술대회
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    • pp.1835-1840
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    • 2004
  • The HANARO, a multi-purpose research reactor of 30 MWth, open-tank-in-pool type, has been under normal operation since its initial criticality in February, 1995. The HANARO is composed of inlet plenum, grid plate, core channel with flow tubes and chimney. The reactor core channel is located at about twelve meters (12 m) depth of the reactor pool and cooled by the upward flow that the coolant enters the lower inlet of the plenum,. rises up through the grid plate and the core channel and comes out from the outlet of chimney. A guide tube is extended from the reactor core to the top of the reactor chimney for easily un/loading a target under the reactor normal operation. But active coolant through the core can be quickly raised up to the top of the chimney through the guide tube by a jet flow. This paper describes an analytical analysis that is the study of the flow behavior through the guide tube under reactor normal operation and unloading the target. As results, it was conformed through the analysis results that the guide jet is suppressed under the top of the chimney after modifying the orifice diameter of 37.5 mm to 31 mm.

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Dynamic Friction of Polyester Air-jet Textured Yarns

  • Rengasamy Raju Seenivasan;Guruprasad Raghavendran;Asis Patnaik
    • Fibers and Polymers
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    • 제6권2호
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    • pp.146-150
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    • 2005
  • In this paper, friction of air-jet textured yams is investigated. Using a friction measuring apparatus fabricated inhouse, dynamic friction forces of the yams under yarn-to-metal (YM) and yam-to-yam (YY) rubbing modes are measured. The influence of processing variables of air-jet texturing viz., overfeed, air pressure, dry/wet texturing and normal/core-and-effect texturing on dynamic friction is analysed. The results indicate that friction force increases with increasing rubbing speeds and yam input tension. YM dynamic friction decreases initially and then starts to increase at higher overfeeds. YY dynamic friction increases with increasing overfeed. YM dynamic friction decreases with an increase in air pressure while an opposite trend is observed for YY friction. Wet textured yams have higher friction than dry textured yams. Core wetted coreand-effect textured yams have higher friction than normal textured yams.