• Title/Summary/Keyword: Closed test section

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Evaporation pressure drop of $CO_2$ in a horizontal tube (수평관내 이산화탄소의 증발 압력강하)

  • Lee Dong-Geon;Son Chang-Hyo;Oh Hoo-Kyu
    • Journal of Advanced Marine Engineering and Technology
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    • v.29 no.5
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    • pp.552-559
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    • 2005
  • The evaporation pressure drop of $CO_2$ (R-744) in a horizontal tube was investigated experimentally. The experiments were conducted without oil in a closed refrigerant loop which was driven by a magnetic gear pump. The main components of the refrigerant loop are a receiver, a variable-speed pump. a mass flow meter, a pre-heater and evaporator (test section). The test section consists of a smooth. horizontal stainless steel tube of 7.75 mm inner diameter. The experiments were conducted at mass flux of 200 to $500\;kg/m^{2}s$, saturation temperature of $-5^{\circ}C\;to\;5^{\circ}C$. and heat flux of 10 to $40\;kW/m^2$. The test results showed the evaporation pressure drop of $CO_2$ are highly dependent on the vapor qualify, heat flux and saturation temperature. The evaporation pressure drop of $CO_2$ is very lower than that of R-22. In comparison with test results and existing correlations. the best fit of the present experimental data is obtained with the correlation of Choi et al. But existing correlations failed to predict the evaporation pressure drop of $CO_2$. Therefore, it is necessary to develop reliable and accurate predictions determining the evaporation pressure drop of $CO_2$ in a horizontal tube.

Study on the Evaporation Heat transfer of $CO_2$ in a Horizontal tube (수평관내의 $CO_2$의 증발 열전달에 관한 연구)

  • Jang, Seong-Il;Choi, Sun-Muk;Kim, Dae-Hui;Oh, Hoo-kyu
    • Proceedings of the Korean Society of Marine Engineers Conference
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    • 2005.11a
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    • pp.240-241
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    • 2005
  • The experiments were conducted without oil in a closed refrigerant loop which was driven by a magnetic gear pump. The main components of the refrigerant loop are a receiver, a variable-speed pump, a mass flow meter, a pre-heater and evaporator(test section). The test section was made of a horizontal stainless steel tube with the inner diameter of 4.57 mm, and length of 4 m. The experiments were conducted at mass flux of 200 to 700 kg/$m^2s$, saturation temperature of 0$^{circ}C$ to 20$^{circ}C$, and heat flux of 10 to 30 kW/$m^2$. The test results showed the evaporation heat transfer of $CO_2$ has great effect on more nucleate boiling than convective boiling. The evaporation heat transfer coefficients of $CO_2$ are highly dependent on the vapor quality, heat flux and saturation temperature. In comparison with test results and existing correlations, correlations failed to predict the evaporation heat transfer coefficient of $CO_2$, therefore, it is necessary to develop reliable and accurate predictions determining the evaporation heat transfer coefficient of $CO_2$ in a horizontal tube.

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Evaporative Heat Transfer Characteristics of Carbon Dioxide in a Horizontal Tube (수평관내 이산화탄소의 증발 열전달 특성)

  • Son Chang-Hyo;Lee Dong-Gun;Kim Young-Lyoul;Oh Hoo-Kyu
    • Korean Journal of Air-Conditioning and Refrigeration Engineering
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    • v.16 no.12
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    • pp.1134-1139
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    • 2004
  • The evaporative heat transfer coefficient of $CO_2$ (R-744) in a horizontal tube was investigated experimentally. The experiments were conducted without oil in a closed refrigerant loop which was driven by a magnetic gear pump. The main components of the refrigerant loop are a receiver, a variable-speed pump, a mass flow meter, a pre-heater and evaporator (test section). The test section consists of a smooth, horizontal stainless steel tube of inner diameter of 7.75 mm. The experiments were conducted at mass flux of 200 to 500 kg/m$^2$s, saturation temperature of -5 to 5$^{\circ}C$, and heat flux of 10 to 40kW/m$^2$. The test results showed the heat transfer of $CO_2$ has a greater effect on nucleate boiling more than convective boiling. Mass flux of $CO_2$ does not affect nucleate boiling too much, and the effect of mass flux on evaporative heat transfer of $CO_2$ is much smaller than that of refrigerant R-22 and R-134a. In comparison with test results and existing correlations, correlations failed to predict the evaporative heat transfer coefficient of $CO_2$, therefore, it is necessary to develope reliable and accurate predictions determining the evaporative heat transfer coefficient of $CO_2$ in a horizontal tube.

A Study on the Heat Transfer Performance of an Energy-Nose Section in a Household Refrigerator-Freezer (가정용 냉장고의 에너지 노즈부 열전달 특성에 관한 연구)

  • Lee, Moo-Yeon;Lee, Dong-Yeon;Kim, Yong-Chan
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.31 no.6 s.261
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    • pp.574-580
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    • 2007
  • The objective of this article is to present an analysis of all heat transfer paths through the energy nose under closed door conditions when refrigeration system of household refrigerator-freezer is operating on. Both experimental and numerical methods are suggested as a means of determining the overall energy nose load amount as well as the load due to each pathway such as mullion section and F and R sides of the household refrigerator-freezer. In other words, all loads determined in this article are just energy nose and not the loads seen by the refrigeration system. We suggest good ideas for improving the heat transfer losses such as conduction and convection through the energy nose. As we can be known from the experimental test results, it is effective to prevent the heat loss of a mullion section. And energy efficiency is also decreased approximately 6% compared to that of a baseline sample test result. As we can be known from the Ansys 8.1 analysis, it is shown the steady state temperature distribution in figures from 6 to 8. And the direction of the heat flow through the energy nose section is also easily seen from that In conclusion, the article is focused on an energy nose section in household refrigerator-freezer for practical proposes which is the energy saving in a household refrigerator-freezer. And the method suggested may be applied to any make or model to aid in the search for high efficient energy nose section of household side by side refrigerator-freezer as well as top mounted refrigerator-freezer, commercial refrigerator and so on.

RESULTS OF THERMAL CREEP TEST ON HIGHLY IRRADIATED ZIRLO

  • Quecedo, M.;Lloret, M.;Conde, J.M.;Alejano, C.;Gago, J.A.;Fernandez, F.J.
    • Nuclear Engineering and Technology
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    • v.41 no.2
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    • pp.179-186
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    • 2009
  • This paper presents a thermal creep test under internal pressure and post-test characterization performed on high burnup (68 MWd/kgU) ZIRLO. This research has been done by the CSN, ENRESA, and ENUSA in order to investigate the behavior of advanced cladding materials in contemporary PWRs at higher burnup under dry cask storage conditions. Also, to investigate the hydride reorientation, the cool-down of the samples after the test has been done in a coordinated manner with the internal pressure. The creep results obtained are consistent with the expected behavior from reference CWSR material, Zr-4. During the test, the material retained significant ductility: one specimen leaked during the test at an engineering strain of the tube section of 17%; remarkably, the crack closed due to de-pressurization. Although significant hydride reorientation occurred during the cool-down under pressure, no specimen failed during the cool-down.

PIV Measurements of Three-Dimensional Wake Around a Road Vehicle (자동차 후류에 대한 3차원 유동의 PIV 측정)

  • Kim Jinseok;Kim Sungcho;Sung Jaeyong;Kim Jeongsoo;Choi Jongwook
    • 한국가시화정보학회:학술대회논문집
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    • 2004.11a
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    • pp.1-4
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    • 2004
  • The PIV measurements are performed to get the quantitative flow visualization around a road vehicle. The model scaled with 1/48 is located in the middle test section of the closed-loop water tunnel and the measuring system consists of CCD camera, diode laser, synchronizer, and computer. The experimental data are obtained at two Reynolds numbers of 50,000 and 100,000 based on the model length. The quasi-three-dimensional isovorticity surfaces, based on two-dimensional velocity field data, are generated. There is little difference between the results in part of the recirculation region and the vorticity contour according to the Reynolds number. Also a little bit complicated three dimensional flows are predicted behind the road vehicle.

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Burning Rate Estimate Method of Solid Propellants at High Pressure Condition (고압에서 작동하는 고체 추진제 연소속도 추정 방법)

  • Choi, Hanyoung;Lee, Dongsun;Sung, Hong-Gye;Lee, Wonmin;Kim, Eunmi
    • Journal of the Korean Society of Propulsion Engineers
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    • v.26 no.1
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    • pp.28-37
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    • 2022
  • The burning rate estimation method of solid propellants, based on closed bomb tests, has been introduced. The composition of the combustion gas is determined by using CEA and the Noble-Abel equation of state for high pressure operation conditions. Covolume taking into account the collision among molecules due to the actual volume of the molecule is modeled by LJ potential. A cubic form function is applied to calculate the volume change of propellant grains during combustion. The estimated burning rates of five different grain configuation at high pressure are fairly compared with BRLCB results within the maximum error of 6%.

Characteristics of Closed Circuit Cooling Tower with Multi Path on Cooling Water Inlet Conditions (냉각수 변화에 따른 멀티패스 밀폐식 냉각탑의 성능)

  • Shim, Gyu-Jin;Baek, Seung-Moon;Moon, Choon-Geun;Yoon, Jung-In;Kim, Eun-Pil;Kwon, O-Ick
    • Proceedings of the SAREK Conference
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    • 2008.06a
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    • pp.597-602
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    • 2008
  • The experiment of performance about closed-wet cooling tower(CWCT) was conducted in this study. The test section has the cooling water that flows from top part of a heat exchanger that has an entrance of cooling water with one and multi path. The heat exchanger consists of 15.88mm tubes with ten rows and ten columns and staggered arrangement. In this experiment, heat and mass transfer coefficients and range are calculated with variations of cooling water and path. The results indicated that operating CWCT using two path have the high values of heat and mass transfer coefficients and range than one path.

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Characteristics of Closed Circuit Cooling Tower with Variation of Tube Diameter (멀티패스 밀폐식 냉각탑의 관경변화 특성)

  • Shim, Gyu-Jin;Lee, Ho-Saeng;Kim, Eun-Pil;Yoon, Jung-In;Kwon, O-Ick
    • Proceedings of the SAREK Conference
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    • 2008.11a
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    • pp.531-536
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    • 2008
  • This paper presents experimental result of characteristics about Closed circuit Cooling Tower having a rated 2RT. The experimental apparatus has been set-up with a conventional type system. The test section is heat exchangers of cooling tower that consist of different vertical tubes, 15.88mm with 10 rows and columns and 19.05 mm with 8 rows and 12 columns. The main results were summarized as follows : The values of heat and mass transfer coefficients of cooling tower operating with two paths are higher than these with one path. Cooling capacity per unit volume using 15.88mm tubes are higher than 19.05mm tubes.

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Elimination of Self Noise & Doppler Effects from the Microphone Array Measurement (마이크로폰 어레이 측정에서의 도플러 효과와 자체소음 제거에 관한 실험적 연구)

  • Rhee, Wook;Park, Sung;Kim, Jai-Moo;Choi, Jong-Soo
    • Transactions of the Korean Society for Noise and Vibration Engineering
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    • v.16 no.7 s.112
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    • pp.677-682
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    • 2006
  • In the case of aeroacoustic test in windtunnel, measurement accuracy is reduced by not only Doppler effects but also by the microphone self noise due to airflow and high turbulence in the wall boundary layer. Microphone array measurements can be easily utilized for the solutions of these problems. In this paper, geometrical optics approach and diagonal term elimination of cross spectral matrix was introduced to the de-dopplerization and self noise reduction methods for the microphone array measurement. For the validation, beamforming tests for sinusoidal point source were performed in the closed type test section of windtunnel, and their performances of beam width and sidelobe rejection were significantly improved.