• Title/Summary/Keyword: Flow test

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Effect of Opening Partition Length on Helium-Air Exchange Flow (개구부 삽입부의 길이가 헬륨 및 공기의 치환류에 미치는 영향)

  • 강태일
    • Journal of Advanced Marine Engineering and Technology
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    • v.23 no.2
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    • pp.192-200
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    • 1999
  • This paper describes experimental investigations of helium-air exchange flow through parti-tioned opening. Such exchange flow may occur following rupture accident of stand pipe in high temperature gas cooled reactor. A test vessel with a opening on top of test cylinder is used for experiments. An estimation method of mass increment is developed and applied to measure the exchange flow rate. A technique of flow visualization by Mach-Zehnder interferometer is provided to recognize the exchange flows. Flow measurements are made with partitioned opening for parti-tion rations $H_p/H_1$ in the range 0 to 1 where $H_p$ and $H_1$ are partition length and height of the open-ing respecticely. In the case of $H_p/H_1$ of 0 flow passages of upward flow of the helium and down-ward flow of the air within the opening are unseparated (bidirectional) and the two flows interact exchange flow rate is minimum through range of the partition ratios, Two flow zones i.e. separat-ed(unidirectional)flow zone and unseparated(bidirectional) flow zone exist with increasing the partition. length, The exchange flow rate increases with increasing the separated flow zone. It is found that a maximum exchange flow rate exists at $H_p/H_1$ of 1. As a result fo comparison of the exchange flow rates by changing the partition ration the fluids interaction in the unseparated zone is found to be an important factor on the helium-air exchange flow rate.

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CATHARE simulation results of the natural circulation characterisation test of the PKL test facility

  • Salah, Anis Bousbia
    • Nuclear Engineering and Technology
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    • v.53 no.5
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    • pp.1446-1453
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    • 2021
  • In the past, several experimental investigations aiming at characterizing the natural circulation (NC) behavior in test facilities were carried out. They showed a variety of flow patterns characterized by an inverted U-shape of the NC flow curve versus primary mass inventory. On the other hand, attempts to reproduce such curves using thermal-hydraulic system codes, showed 10-30% differences between the measured and calculated NC mass flow rate. Actually, the used computer codes are generally based upon nodalization using single U-tube representation. Such model may not allow getting accurate simulation of most of the NC phenomena occurring during such tests (like flow redistribution and flow reversal in some SG U-tubes). Simulations based on multi-U-tubes model, showed better agreement with the overall behavior, but remain unable to predict NC phenomena taking place in the steam generator (SG) during the experiment. In the current study, the CATHARE code is considered in order to assess a NC characterization test performed in the four loops PKL facility. For this purpose, four different SG nodalizations including, single and multi-U-tubes, 1D and 3D SG inlet/outlet zones are considered. In general, it is shown that the 1D and 3D models exhibit similar prediction results up to a certain point of the rising part of the inverted U-shape of the NC flow curve. After that, the results bifurcate with, on the one hand, a tendency of the 1D models to over-predict the measured NC mass flow rate and on the other hand, a tendency of the 3D models to under-predict the NC flow rate.

Study on the Stability Test of Impinging(FOOF) Injector on $GN_2$ Purge Cold Flow Test (질소분사 음향시험을 통한 충돌형(FOOF) 분사기의 안정성 평가에 관한 연구)

  • Yoo Doc-Koon;Lee Kwang-Jin;Seo Seong-Hyeon;Han Young-Min;Choi Hwan-Seok;Seol Woo-Seok
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2006.05a
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    • pp.135-140
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    • 2006
  • In the experimental study of $N_2$ purge cold flow test of impinging(FOOF) injector for determining of instability region, the whistling sound which has a specific frequency is generated. The frequency of whistling is proportional to the gas flow velocity in part of the oxidizer orifice and due to the coupling of the vibrating gas column and the natural frequency of pipe-orifice shape, the discontinuous jumping phenomena arises. The whistling phenomena have no effect on the combustion instability. Compared the damping factor of 1T1L mode with the hot fire test, the instability region of $N_2$ purge cold flow test is very much like that. It means that flow instability by impinging or mixing of jet is the main reason of combustion instability of impinging injector(FOOF) in the hot firing test.

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In -Cylinder Flow Characteristics Varying Intake Valve Lift (밸브 리프트 변화에 따른 실린더 내 흡입 공기의 유동 특성)

  • 윤정의
    • Transactions of the Korean Society of Automotive Engineers
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    • v.7 no.9
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    • pp.82-88
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    • 1999
  • The object of this study is to find new evaluation index for in-cylinder flow chracteristics istead of current swirl, tumble coefficient using steady flow test rig on intake port system. To this end, port flow system. To this end, port flow rig test was conducted on DOHC head varying intake valve lift respectively. Finally combination angular coefficient and inclination angle were introduced as new evaluation index for in-cylinder angularflow characteristics instead of swirl and tumble coefficient.

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A Study on Combined Effects between Swirl and Tumble Flow of Intake Port System in Cylinder Head (엔진 흡입포트 시스템 유동특성 규명을 위한 스월-텀블 합성효과에 관한 연구)

  • 윤정의
    • Transactions of the Korean Society of Automotive Engineers
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    • v.7 no.8
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    • pp.76-82
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    • 1999
  • The object of this study is to find new evalution index for in-cylinder flow characteristics insteady of current swirl, tumble coefficient using steady flow test rig on intake port system. To this end, port flow rig test was conducted on DOHC head varying intake valve lift respectively. Finally combination angular coefficient and inclination angle were introduced as new evaluation index for in-cylinder angular flow characteristics.

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A Study on Development of Vane Damper for Industry Flow Control Fan (산업용 유량제어 송풍기 베인댐퍼 개발에 관한 연구)

  • Yi, Chung-Seob;Jeong, In-Guk;Yun, Ji-Hun;Suh, Jeong-Se;Jang, Sung-Cheol
    • Journal of the Korean Society of Manufacturing Technology Engineers
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    • v.21 no.1
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    • pp.137-143
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    • 2012
  • In this study, it was conducted to design each components of vane damper for industrial flow control fan and the flow rates were analysed by experimental and numerical method. Through environmental test, it could be confirmed that the designed vane damper was appropriate. Also, almost identical results with test could be drawn from numerical method. Finally, flow rates of electric and pneumatic actuator were measured by test. As the results, difference of flow rate according to opening ratio was smaller in pneumatic actuator than that in electric actuator.

Development of Flow Control Valves for Hot Water Distribution Manifolds (온수분배기용 유량제어밸브의 개발)

  • Kwon, Woo-Chul;Yoon, Joon-Yong;Yoo, Sun-Hak
    • The KSFM Journal of Fluid Machinery
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    • v.13 no.4
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    • pp.11-17
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    • 2010
  • The developed control valves, installed on the hot water distribution manifolds for the floor heating system, consist of the balancing valves and the shut-off valves. The balancing valve was designed to improve the flow control performance and to reduce the noise emitted from the valve by modification of the general V port. The port of the shut-off valve was designed with two ceramic plates, working by rotating upper plate, to improve the duration and to reduce the noise. For the evaluation of the new valves, the flow rate was measured and noise level test was carried out. The test results showed that the error of the flow rate accuracy test for the flow balance of each manifold circuit was less than ${\pm}3%$ and the noise level was less than 35 dB(A).

Wind Tunnel Test of 2D Model for Plasma Flow Control using DBD Plasma Actuator (DBD 플라즈마 구동기를 이용한 2차원 모델의 플라즈마 유동제어 풍동시험)

  • Yun, Su-Hwan;Kim, Tae-Gyu
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2012.05a
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    • pp.527-528
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    • 2012
  • DBD (Dielectric Barrier Discharge) plasma actuator was designed for aerodynamic drag reduction using plasma flow control, and the drag reduction was measured by wind-tunnel tests using 2D test model. At the zero wind velocity, the plasma flow control had no effect on the drag reduction because the flow separation and surface friction drag were not occurred. At the wind velocity of 2m/s, 9.7% of drag was reduced by the flow separation control. The drag reduction decreased as the wind velocity increased.

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Critical Heat Flux and Flow Pattern for Water Flow in Annular Geometry

  • Park, Jae-Wook;Baek, Won-Pil;Chang, Soon-Heung
    • Proceedings of the Korean Nuclear Society Conference
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    • 1996.11a
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    • pp.224-229
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    • 1996
  • An experimental study on critical heat flux (CHF) and two-phase flow visualization has been performed for water flow in internally-heated, vertical, concentric annuli under near atmospheric pressure. Tests have been done under stable forced- circulation, upward and downward flow conditions with three test sections of relatively large gap widths (heated length = 0.6 m. inner diameter = 19 mm, outer diameter = 29, 35 and 51 mm). The outer wall of the test section was made up of the transparent Pyrex tube to allow the observation of flow patterns near the CHF occurrence. The CHF mechanism was changed in the order of flooding, chum-to-annular flow transition, and local dryout under a large bubble in churn flow as the flow rate was increased from zero to higher values. Observed parametric trends are consistent with the previous understanding except that the CHF for downward flow is considerably lower than that for upward flow.

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A Numerical Study on the Flow Uniformity according to Chamber Shapes Used for Test of the Semi-Conductor Chip (반도체 칩 테스트용 챔버 형상에 따른 유동 균일성에 대한 수치적 연구)

  • LEE, DAEGYU;MA, SANG-BUM;KIM, SUNG;KIM, JEONG-YEOL;KANG, CHAEDONG;KIM, JIN-HYUK
    • Transactions of the Korean hydrogen and new energy society
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    • v.31 no.5
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    • pp.480-488
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    • 2020
  • This study was conducted to improve the flow uniformity inside the chip tester through changing the flow path formation according to the inlet and outlet position of chamber. The internal flow and velocity distributions of the modified chamber models (Cases 1-3) were compared with the reference chamber model through three-dimensional Reynolds-averaged Navier-Stokes equations with k-ε turbulence model. The modified chamber models showed the superior flow uniformity characteristics compared to the reference chamber model. To investigate the flow uniformity in the chip tester, the standard deviation of the velocity was defined and compared. Through the internal flow analysis and assesment of the standard deviation, Case 2 among the test cases including the reference model showed the best flow uniformity generally.