• Title/Summary/Keyword: Square Rod

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Effect of Heat Transfer Augmentation by Square Rod Array in Impinging Air Jet System(Heat Transfer Characteristic of Potential Core Region) (충돌공기분류계에서 사각 ROD에 의한 전열증진 효과(포텐셜코어영역에서의 전열특성))

  • Kum, Seong-Min;Oh, Soo-Cheol;Seo, Jeong-Yoon
    • Solar Energy
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    • v.15 no.1
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    • pp.85-94
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    • 1995
  • This research has been proceeded over the potential core region(H/B=2) of two-dimensional impinging air jet sytem, in which square rods(width of 6 mm) has been set up in front of heating surface in order to increase heat transfer. The objective of this research was to investigate the characteristics of heat transfer and air flow, in eases of the clearance from rods to heating surface(C=1, 2, 4, 6 mm) and the pitch between each rods(P=30, 40, 50 mm) changed. And this research compared the above with the experimentation without rods. As result, heat transfer performance was best under the condition of C=1mm, in case clearance changed, and there was no serious difference in the effect of heat transfer augmentation in the case of pitch of rods changed.

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Thermal-Hydraulic Aspects of an Advanced Reactor Core with Triangular Lattice Fuel Assemblies

  • Hwang, Dae-Hyun;Yoo, Yeon-Jong;Kim, Young-Jin;Chang, Moon-Hee
    • Proceedings of the Korean Nuclear Society Conference
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    • 1996.05b
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    • pp.379-384
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    • 1996
  • Thermal-hydraulic performance has been analyzed for an advanced reactor core loaded with hexagonal fuel assemblies. Currently available CHF prediction models and data base for triangular lattice bundles have been thoroughly reviewed, and as a result the KfK-3 CHF correlation with limit CHFR of 1.235 has been determined to be most appropriate. The pressure drop model in COBRA-IV-I code has been modified for the analysis of triangular lattice rod bundles. In view of maximizing the thermal margin, the geometry of a hexagonal fuel assembly, such as rod diameter and rod pitch, has been optimized with a fixed fuel assembly cross sectional area The optimum value of the moderator-to-fuel volume ratio is estimated to lie between 0.65 to 1 with 9.5 mm rod diameter. The thermal margin of these hexagonal fuel assemblies in the AP600 core has been evaluated and compared with that of square lattice fuel assemblies such as VANTAGE-5H and KOFA. The analysis result shows that the performances of hexagonal fuel assemblies are more favorable than the square fuel assemblies in the aspect of steady-state overpower margin.

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Thermal Flow Characteristics of Impinging Air Jet by Shape of Turbulence Promoter (난류촉진체 형상에 의한 충돌제트의 열유동 특성)

  • Kum, Sungmin;Jho, Shigie;Yu, Byeonghun;Lee, Seungro
    • Journal of Energy Engineering
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    • v.21 no.2
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    • pp.187-193
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    • 2012
  • In this study, it was experimentally investigated the effect of the clearances distance between the rod and the impinging plate on characteristics of the thermal flow. For the heat transfer enhancement of wall jet region, the right triangle and the square rods were arranged in front of the impinging plate with various clearance distances. As results, the heat transfer enhancement rate of potential core region at H/B=2 was higher than that of transition region at H/B=10. In this experiment range, the maximum heat transfer enhancement rate was about 46 % higher at the square rod with H/B=2 and C=1mm compared with the flat plate. The heat transfer enhancement rate of the right triangle rod was on average about 3 to 8 % higher than that of the square rod, regardless of the clearance.

A Study on the Measurement of the Fluid Viscosity by Using the Torsional Vibration of a Circular Rod (원형 봉의 비틀림 진동에 의한 유체 점도 측정 연구)

  • Chun, Han-Yong;Kim, Jin-Oh
    • Transactions of the Korean Society of Mechanical Engineers A
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    • v.26 no.6
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    • pp.1016-1025
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    • 2002
  • This paper deals with the measurement of the fluid viscosity by using the torsional vibration of a circular rod excited by a torsional vibrator at one end. The effect of an adjacent viscous fluid on the torsional vibration of the rod has been studied theoretically and expressed in terms of the mechanical impedance. The theoretically-obtained trend that the mechanical impedance is proportional to the square root of the viscosity times the density of the fluid has been confirmed by the impedance measurement. The paper demonstrates that a torsionally-vibrating rod can be used as a sensor to measure the viscosity of a fluid.

A Study on the Corner Filling in the Drawing of the Rectangular Rod (사각재 인발 공정의 코너채움에 관한 연구)

  • Kim Y. C.;Kim Y. S.;Kim B. M.
    • Proceedings of the Korean Society for Technology of Plasticity Conference
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    • 1999.05a
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    • pp.56-59
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    • 1999
  • In the present study, in order to investigate the effect of the corner filling in the drawing of the rectangular rod from a round bar, the drawing of the square rod from a round bar has been simulated by using rigid-plastic finite element method and artificial neural network has been introduced to reduce the number of simulation. The experimental investigation has been also implemented to verify the efficiency of the application of results of present and previous study. According to the results of present and pervious study, the combination of semi-die angle gives a great effect on the corner filling in case of the irregular shaped drawing process, but, in case of the regular shaped drawing process, the main process variable on the corner filling is reduction in area.

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The Interaction Between the Torsional Vibration of a Circular Rod and an Adjacent Viscous Fluid (원형 봉의 비틀림 진동과 인접 점성유체의 상호작용)

  • Chun, Han-Yong;Kim, Jin-Oh
    • Proceedings of the KSME Conference
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    • 2001.06b
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    • pp.378-385
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    • 2001
  • This paper deals with the effect of an adjacent viscous fluid on the torsional vibration of a circular rod excited by a transducer at one end. The interaction between the torsional vibration of the rod and the fluid has been studied theoretically and expressed in terms of the mechanical impedance. The theoretically-obtained trend that the mechanical impedance is proportional to the square root of the viscosity times density of the fluid has been confirmed by the impedance measurement. The paper demonstrates that a torsionally-vibrating rod can be used as a sensor measuring the viscosity of a fluid.

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A New Design Procedure for the Evaluation of Rod Bow DNBR Penalty

  • Paik, Hyun-Jong;Yang, Seung-Geun
    • Nuclear Engineering and Technology
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    • v.28 no.3
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    • pp.331-338
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    • 1996
  • In the thermal-hydraulic design, the effect of fuel rod bow is quantified tv the rod bow DNBR penalty which is a key design parameter to assure the coolability of fuel assembly in the pressurized water reactor. In this work, a computer program for the evaluation of the rod bow DNBR penalty based on Westinghouse methodology is developed and its application procedure is proposed. The computer simulation is based on the Monte-Carlo method. The qualification of developed computer program is performed by a comparison of calculational result with that given by Westinghouse's document. A new application procedure is built using batch mean and batch standard deviation. The normality of sample population generated by the batch calculation is confirmed by means of a chi-square test for goodness of fit. On the view point of statistics it is effected that the more reliable design value may be produced by the new application procedure.

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A CORRELATION FOR SINGLE PHASE TURBULENT MIXING IN SQUARE ROD ARRAYS UNDER HIGHLY TURBULENT CONDITIONS

  • Jeong, Hae-Yong;Ha, Kwi-Seok;Kwon, Young-Min;Chang, Won-Pyo;Lee, Yong-Bum
    • Nuclear Engineering and Technology
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    • v.38 no.8
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    • pp.809-818
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    • 2006
  • The existing experimental data related to the turbulent mixing factor in rod arrays is examined and a new definition of the turbulent mixing factor is introduced to take into account the turbulent mixing of fluids with various Prandtl numbers. The new definition of the mixing factor is based on the eddy diffusivity of energy. With this definition of the mixing factor, it was found that the geometrical parameter, ${\delta}_{ij}/D_h$ correlates the turbulent mixing data better than Sid, which has been used frequently in existing correlations. Based on the experimental data for a highly turbulent condition in square rod arrays, a correlation describing turbulent mixing dependent on the parameter ${\delta}_{ij}/D_h$ has been developed. The correlation is insensitive to the Re number and it takes into account the effect of the turbulent Prandtl number. The proposed correlation predicts a reasonable mixing even at a lower S/d ratio.

An Experimental Study on the Cooling Effect by a Turbulence Promoter in Impinging Air Jet System (충돌분류계(衝突噴流系)에서 난류촉진체(亂流促進體)에 의한 방열효과(放熱效果)에 관(關)한 연구(硏究))

  • Lee, Y.H.;Seo, J.Y.
    • Korean Journal of Air-Conditioning and Refrigeration Engineering
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    • v.4 no.1
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    • pp.48-56
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    • 1992
  • The purpose of this study was to investigate the enhancement of heat transfer without additional external power in the case of rectangular air jet impinging vertically on the flat heating surface. In an attempt to enhance the heat transfer rate in two-dimensional impinging jet, the technique used in the present study was placement of square rod bundles as a turbluence promoter in front of the heat transfer surface. The effects of the clearance between the flat plate and square rod, and the nozzle exit velocity on the heat transfer characteristics have been investigated experimentally. The results obtained through this study were summerized as follows. High heat transfer enhancement was achived by means of flow acceleration and thinning of boundary layer by inserting rods in front of the heating flat plate. The smaller the clearance between rod and heating plate was, the larger heat transfer effect became. Average Nusselt number reached maximum at $Re=5.76{\times}10^4$ and C=1㎜ and the enhancement rate of heat transfer became maxium at this condition with the enhancement ratio as high as about 1.427 when normalized by the flat plate value. The correlating equation of average Nusselt number and Reynolds number was obtained, which is $\bar{N}uo=1.324{\cdot}Re^{0.459}{\cdot}(C/A)^{-0.034}$.

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