• The KSFM Journal of Fluid Machinery
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• v.2 no.3 s.4
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• pp.37-44
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• 1999

In a screw-type centrifugal pump, the pump head deteriorates from single-phase flow to the choke due to an increased air entrainment at a wide tip clearance compared to that of a narrow tip clearance. Moreover, at a narrow tip clearance, the pump head became partially higher in a two-phase flow than that of a single-phase flow near the best efficiency point in low void fraction region. Therefore, we observed the internal flow pattern by using a stroboscope and we measured the mean size of bubbles from the images obtained with a high speed camera. Then, we investigated the influences of the mean size of bubbles, tip clearances and flow patterns on pump performance.

• Korean Journal of Air-Conditioning and Refrigeration Engineering
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• v.10 no.2
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• pp.238-250
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• 1998

Vapor-liquid equilibrium apparatus is designed and set up. The vapor-liquid equilibrium data of the binary system HFC125/134a are measured in the range between 268.15 and 283.15K at five compositions. Twenty-five equilibrium data are obtained. To verify consistency of these data, they are tested for thermodynamic consistency. Based upon the present data, the binary interaction parameter for CSD and RKS equation of state is calculated at five isotherms and comparison with the data in the open literatures is made. Results of Nagel and Bier are in very good agreements with those from this study within 0.32∼1.11% for bubble point pressure and －0.66∼0.18% for vapor mole fraction.

• Proceedings of the Membrane Society of Korea Conference
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• 1996.10a
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• pp.59-59
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• 1996

막분리에 의한 폐윤활유 재생공정을 개발하기 위한 기초 연구로써 폐윤활유 분리/재생용으로 적합한 복층(multilayer)세라믹 복합막의 제조와 합성막의 폐유 분리 효율등이 연구되었다. 결함이 없고 두께가 균일한 지르코니아 복합막 (기공크기 0.07 $\mu$m 이하)은 압출 성형법으로 제조한 튜브형 $\alpha$-알루미나 담체 (외경 7.8 mm, 두께 0.6 mm, 기공크기 0.7 $\mu$m)내부표면에 역침지 인상법(reverse dip-drawing technique)에 의하여 지르코니아 슬러리를 코팅 한 후 950$\circ$C에서 1시간 열처리하여 제조 되었다. 또한 지르코니아 복합막 위에 니타니아 졸-겔 코팅을 한 후 450$\circ$C에서 2시간 열처리하여 기공크기가 15 nm정도인 3층 복합막을 제조 하였다. SEM, Bubble Point Test, Mercury Porosimeter 그리고 분획 분자량 측정등에 의하여 복합막의 코팅층 두께, 결함유무 및 막의 기공크기등을 분석하였다.

• Progress in Superconductivity and Cryogenics
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• v.15 no.3
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• pp.20-23
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• 2013

In the development of high temperature superconducting (HTS) power machines, HTS bushing is one of core technologies. In particular, the insulation body with sheds and electrical insulation at cryogenic temperature have attracted a great deal of interest from the view point of the size, weight and efficiency of bushing. In this study, the electrical and mechanical characteristics of various insulators for body in liquid nitrogen ($LN_2$) were investigated. And the surface discharge distance, collar length of GFRP sheds were studied. To emit bubbles between sheds, the shape and arrangement of shed were studied. The shed structure for 60 kV class HTS bushing were designed with regular arrangement.

• Journal of computational fluids engineering
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• v.15 no.3
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• pp.1-8
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• 2010

Laminar separation bubble and transitional flow over the NACA0012 are investigated at a moderate range of Reynolds numbers. A Reynolds-Averaged Navier-Stokes code is coupled with an empirical transition model that can predict transition onset points and the length of transition region. Without solving the boundary layer equations, approximated e-N method is directly applied to the RANS code and iteratively solved together. The computational results are compared with the experimental data for the NACA0012 airfoil. Results of transition onset point and the length are compared well with experimental data and Xfoil prediction. The present RANS results show at high angles of attack better agreement with experimental data than Xfoil results using the boundary layer equations.

• Journal of Advanced Marine Engineering and Technology
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• v.26 no.1
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• pp.83-89
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• 2002

In the present study, heat transfer characteristics of oil flow over offset strip fins were predicted by the numerical methods. Oil flow in the plate-fin passage was idealized by 2 dimensions. The flow patterns and heat transfer characteristics were predicted in details. Numerical results shows that the average convective heat transfer coefficients are almost independent on the raws of fins and affected by fin pitches. At the rear face of fin, there exists minimum point of heat transfer coefficients where stream are separated from the fin surfaces. The convective heat transfer coefficients were effected by separation bubbies which appeared at the wake region of offset strip fins.

• Journal of Advanced Marine Engineering and Technology
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• v.17 no.2
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• pp.36-43
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• 1993

Real quality and axial void fraction distribution of subcooled refrigerant flow is very important to predict the heat transfer rate and pressure drop in the design of refrigerating system. In the subcooled boiling region, the liquid bulk temperature is still below the corresponding saturation temperature. But beyond the net vapor generation point, bubble detachment is occured actively from the vapor layer formed on the wall. A reliable method to predict the vapor fraction from the liquid bulk temperature is suggested in this paper. And also the actual quality of the subcooled R-113 flow is calculated in the range of 261-1239kg/$m^2$s mass velocity and 10-30K subcooling.

• Proceedings of the Membrane Society of Korea Conference
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• 1994.10a
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• pp.80-80
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• 1994

세라믹막을 이용한 oil 폐수 처리의 기초 연구로서 정밀여과용 세라믹막의 제조와 oil(kerosene)-in-water 타입 에멀젼에 대한 막분리 효율이 연구되었다. 정밀여과 막으로서는 압출(extrusion)법으로 성형하여 제조한 $\alpha$-알루미나 튜브(평균 기공크기 0.9 $\mum$)와 이들 튜브(담체)내부에 $ZrO_2$ 또는 $Al_2O_3$ 다공성 박막을 코팅한 2층 구조의 복합막들을 사용하였다. 담체의 높은 투과율 ($1700 l/m^2\cdot h$ at $\Deltap = 1$ atm)을 어느정도 유지하면서 막분리 효율을 증대시킬 수 있는 새로운 슬러리 코팅법이 개발되엇으며, 코팅후 950-1300$\circ$C 에서 열처리한 코팅층의 두께와 평균 기공크기는 각각 5 - 20 $\mum$정도 이었다. 정밀여과막의 특성평가를 위하여 막 제조조건에 따른 코팅층의 두께 및 결함유무를 SEM으로 일단 관찰한 후에 Bubble Point Test와 Mercury Porosimeter를 이용하여 측정한 최대 및 평균 기공반경과 물의 투과량으로부터 막 전체에 대한 결함 유무와 결함의 허용한도등을 비교 분석하였다.

• Korean Journal of Air-Conditioning and Refrigeration Engineering
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• v.12 no.11
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• pp.1031-1037
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• 2000

Isothermal vapor-liquid equilibrium(VLE) data have been obtained for the systems of propane(R290)+1,1,1,2-tetrafluoroethane(R134a) and 1,1,1,2-tetrafluoroethane(R134a)+isobutane(R60A) in the temperature range of 253.15 to 323.15K. Experiments were performed in a circulation type apparatus by injecting vapor through liquid pool using a magnetic pump. Both systems form azeotropes in the temperature range of this study. The experimental results were estimated with the Peng-Robinson equation of state. When the temperature-dependent binary interaction parameter was used in the Peng-Robinson equation of state, the absolute average deviation of the measured bubble point pressures from the values correlated by the Peng-Robinson equation was 0.65% and 0.78% for R290+R134a and R134a+600a, respectively. Azeotropic compositions for both systems were presented.

• Korean Journal of Air-Conditioning and Refrigeration Engineering
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• v.9 no.4
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• pp.527-535
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• 1997

Vapor-liquid equilibrium apparatus is designed and set up. The vapor-liquid equilibrium data of the binary system HFC32/134a are measured in the range between 258.15 and 283.15K at compositions of 0.2, 0.4, 0.6 and 0.8 mole fraction of HFC32. Twenty-two equilibrium data are obtained. Based upon the present data, the binary interaction parameter for Carnahan-Starling-De Santis equation of state is calculated. Temperature range of data is extended to 313.04K using the data in the open literatures. Interaction parameters are determined at nine isotherms.