• 한국강구조학회 논문집
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• 제29권3호
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• pp.205-215
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• 2017

본 연구에서는 10MW급 풍력하중을 받는 멀티기둥 타워시스템에 원형강관 부재의 구조안전성 및 경제성을 함께 검토하는 방식으로 부재 유용도에 근거한 개념설계의 예를 보였다. 단일 실린더형 타워를 대체할 수 있는 멀티기둥타워 구조의 구성에 관한 기본적인 가정을 정립하였고, 그에 따라 제안된 구조물을 모델링하고 해석하여 부재력을 확인하였다. 산정된 부재강도와 작용하중을 근간으로 제안된 멀티기둥타워의 각 부재별로 축력, 전단, 휨, 비틂에 대한 유용도가 산정되었고, 풍력타워로서의 적합성이 평가하였다. 멀티기둥 풍력타워의 개념설계에 채택될 수 있는 수준의 유용도 범위에서 강관 치수, 세장비 및 수평재 단수 등의 설계 매개변수를 제안하였다.

• 열처리공학회지
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• 제16권6호
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• pp.320-328
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• 2003

A specimen of Cu-35%Sn alloy has been subjected to the unidirectional heat treatment in an attempt to examine the evolution of microstructures under varying thermal conditions. The specimen was cast in the form of a cylinder 10 mm in diameter and 200 mm in length, which was then installed in the temperature gradient field established inside a vertical tube furnace. The furnace temperature was adjusted to make the upper part at $750^{\circ}C$ and bottom end part at $300^{\circ}C$ of the specimen. The experiment was terminated by dropping it into water after the 30 minutes holding at given temperature. By the rapid cooling, the high temperature phases, ${\gamma}$ and ${\zeta}$, were retained at ambient temperature with some of ${\gamma}$ phase transformed to ${\varepsilon}$ phase, especially at the grain boundaries of ${\gamma}$ phase. The presence of ${\varepsilon}$ phase was found to determine the nature of phase transformations of the ${\zeta}$ phase undergoes upon cooling. In the close area of the ${\varepsilon}$ phase, ${\varepsilon}$ phase grew separately out of ${\zeta}$, and adds to the preexisting ${\varepsilon}$ whereas in areas away from ${\varepsilon}$, both ${\delta}$ and ${\varepsilon}$ grew simultaneously out of ${\zeta}$, and formed a lamella eutectoid structure. The transformation to ${\delta}$ was found to occur only in slow cooling. The hardness on each phase showed that the retained phases, ${\gamma}$ and ${\zeta}$, could be plastically deformed without brittle fracture while the phases, ${\varepsilon}$ and ${\delta}$, were too brittle to be deformed.

• 생물환경조절학회지
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• 제18권3호
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• pp.200-207
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• 2009

This study was conducted to analyze the variations of air temperature, relative humidity and pressure in a low pressure chamber for plant growth. The low pressure chamber was composed of an acrylic cylinder, a stainless plate, a mass flow controller, an elastomer pressure controller, a read-out-box, a vacuum pump, and sensors of air temperature, relative humidity, and pressure. The pressure leakage in the low pressure chamber was greatly affected by the material and connection method of tubes. The leakage rate in the low pressure chamber with the welding of the stainless tubes and a plate decreased by $0.21kPa{\cdot}h^{-1}$, whereas the leakage in the low pressure chamber with teflon tube and rubber O-ring was given by $1.03kPa{\cdot}h^{-1}$. Pressure in the low pressure chamber was sensitively fluctuated by the air temperature inside the chamber. An elastomer pressure controller was installed to keep the pressure in the low pressure chamber at a setting value. However, inside relative humidity at dark period increased to saturation level.. Two levels (25 and 50kPa) of pressure and two levels (500 and 1,000sccm) of mass flow rate were provided to investigate the effect of low pressure and mass flow rate on relative humidity inside the chamber. It was concluded that low setting value of pressure and high mass flow rate of mixed gas were the effective methods to control the pressure and to suppress the excessive rise of relative humidity inside the chamber.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2002년도 학술대회지
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• pp.687-690
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• 2002

Multimode boundary-layer transition on a NACA0012 airfoil is experimentally investigated under periodically passing wakes and the moderate level of free-stream turbulence. The periodic wakes are generated by rotating circular cylinders clockwise or counterclockwise around the airfoil. The free-stream turbulence is produced by a grid upstream of the rotating cylinder, and its intensity(Tu) at the leading edge of the airfoil is $0.5\;or\;3.5\;{\%}$. The Reynolds number ($Re_c$) based on chord length (C) of the alrfoil is $2.0{\times}10^5$, and Strouhal number ($St_c$) of the passing wake is about 0.7. Time- and phase-averaged streamwise mean velocities and turbulence fluctuations are measured with a single hot-wire probe, and especially, the corresponding wall skin friction is evaluated using a computational Preston tube method. The wake-passing orientation changes pressure distribution on the airfoil in a different manner irrespective of the free-stream turbulence. Regardless of free-stream turbulence level, turbulent patches for the receding wakes propagate more rapidly than those for the approaching wake because adverse pressure gradient becomes larger. The patch under the high free-stream turbulence ($Tu=3.5{\%}$) grows more greatly in laminar-like regions compared with that under the low background turbulence ($Tu=0.5{\%}$) in laminar regions. The former, however, does not greatly change the original turbulence level in the very near-wall region while the latter does it. At further downstream, the former interacts vigorously with high environmental turbulence inside the pre-existing transitional boundary layer and gradually lose his identification, whereas the latter keep growing in the laminar boundary layer. The calmed region is more clearly observed under the lower free-stream turbulence level and for the receding wakes. The calmed region delays the breakdown further downstream and stabilizes more the boundary layer.

• Journal of Mechanical Science and Technology
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• 제15권3호
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• pp.291-299
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• 2001

Recently, severe wear on the shutdown rod cladding of Ulchin Nuclear Power Plant #1, #2 were observed by the Eddy Current Test(E.C.T.). In particular, the wear at the sixth card location was up to 75%. The test results indicated that the Flow Induced Vibration(F.I.V.) might be the cause of the fretting wear resulting from the contact between Rod Cluster Control Assemblies(RCCAs) and their spacing cards(guide plates) arranged in the guide tube. From reviewing RCCAs fretting wear repots and analyzing the general characteristics of F.I.V. mechanism in the reactor, geometric layout and flow conditions around the control rod, it is concluded that the turbulence excitation is the most probable vibration mechanism of RCCA. To identify the governing mechanism of RCCA vibration, an experiment was performed for a representative rod position in which the most serious fretting wear experienced among the six rod positions. The experimental rig was designed and set up to satisfy the governing nondimensional numbers which are Reynolds number and mass damping parameter. The vibration amplitude measurement by the non-contact laser displacement sensor showed good agreements in the frequency and the maximum wearing(vibration) location with Ulchin E.C.T. results and Framatome report, respectively. The sudden increase in the vibration amplitude was sensed around the 6th guide plate with mass flow rate variation. Comparing the similitude rod behaviour with the idealized response of a cylinder in flow induced vibration, it was found that he dominant mechanism of vibration was transferred from turbulence excitation to periodic shedding at the mass flow ate 90ι/min. Also the critical velocity of the vibration in RCCAs was determined and the vibration can be prevented by reducing the bypass flow rate below the critical velocity.

• 대한기계학회논문집B
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• 제30권9호
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• pp.921-928
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• 2006

Wake-induced boundary-layer transition on a NACA0012 airfoil with zero angle of attack is experimentally investigated in periodically passing wakes under the moderate level of free-stream turbulence. The periodic wakes are generated by rotating circular cylinders clockwise or counterclockwise around the airfoil. The free-stream turbulence is produced by a grid upstream of the rotating cylinder, and its intensities $(Tu_{\infty})$ at the leading edge of the airfoil are 0.5 and 3.5%, respectively. The Reynolds number (Rec) based on chord length (C) of the airfoil is $2.0{\times}10^5$, and Strouhal number (Stc) of the passing wake is about 1.4. Time- and phase-averaged streamwise mean velocities and turbulence fluctuations are measured with a single hot-wire probe, and especially, the corresponding wall skin friction is evaluated using a computational Preston tube method. The patch under the high free-stream turbulence $(Tu_{\infty}=3.5%)$ grows more greatly in laminar-like regions compared with that under the low turbulence $(Tu_{\infty}=0.5%)$ in laminar regions. The former, however, does not greatly change the turbulence level in very near-wall region while the latter does it. At further downstream, the former interacts vigorously with high environmental turbulence inside the pre-existing transitional boundary layer and gradually loses its identification, whereas the latter keeps growing in the laminar boundary layer. The calmed region is more clearly observed under the lower free-stream turbulence level and with the receding wakes.

• 태양에너지
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• 제15권1호
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• pp.3-11
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• 1995

본 연구는 수평원통내에 물을 체적비($V_l/V_{tot}$) 0.50, 0.91로 각각 장입한 후 물의 조기 과열온도와 벽면 냉각온도를 각각 변화시키면서 내향 응고시켰을 경우, 시간에 따른 상변화물질의 평균온도, 상경계면의 형상, 응고율, 응고에너지 등을 실험적으로 구하여 이를 비교 검토한 것이다. 응고진행시 상경계면은 물의 초기 과열온도가 높을수록 응고초기에 상단부분이 하단부분보다 빠르게 진행되었으나 응고가 진행됨에 따라 상하단의 상격계면 전진속도는 거의 동일하게 나타났다. 동일한 온도조건에서 전과정에 걸친 응고율($M_s/M_{tot}$)은 체적비 0.5인 경우가 0.91인 경우 보다 크게 나타나 수평원통내 물의 내향응고시 물의 체적비($V_l/V_{tot}$) 변화에 의한 영향도 고려하여야 함을 알 수 있었다.

• 산업기술연구
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• 제18권
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• pp.249-258
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• 1998

In this paper, we investigated the post-combustion removal of nitrogen oxide($NO_x$) and sulfur oxide($SO_x$) which is based on the gas to particle conversion process by the pulsed corona discharge. Under normal pressure, the pulsed corona discharge produces the energetic free electrons which dissociate gas molecules to form the active radicals. These radicals cause the chemical reactions that convert $SO_x$ and $NO_x$ into acid mists and these mists react with $NH_3$ to form solid particles. Those particles can be removed from the gas stream by conventional devices such as electrostatic precipitator or bag filter. The reactor geometry was coaxial with an inner wire discharge electrode and an outer ground electrode wrapped on a glass tube. The simulated flue gas with $SO_x$ and $NO_x$ was used in the experiment. The corona discharge reactor was more efficient in removing $SO_x$ and $NO_x$ by adding $NH_3$ and $H_2O$ in the gas stream. We also measured the removal efficiency of $SO_x$ and $NO_x$ in a cylinder type corona discharge reactor and obtained more than 90 % of removal efficiency in these experimental conditions. The effects of process variables such as the inlet concentrations of $SO_x$, $NH_3$ and $H_2O$, residence time, pulse frequencies and applied voltages were investigated.

• 구강회복응용과학지
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• 제26권3호
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• pp.311-322
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• 2010

본 연구는 최근 심미수복에 흔히 사용되는 IPS e.max Press와 각종 레진 시멘트간의 결합강도를 알아보고자 하였다. 직경 12mm, 높이 3mm의 원반형 IPS e.max Press 시편을 제조사의 지시에 따라 만들어 초음파로 세척하여 자가중합 아크릴릭 레진에 포매하였다. 플라스틱 튜브를 사용하여 직경 4.5mm, 높이 3mm의 40개의 원주형 레진 시편을 제작하였다. 각각의 시편은 무작위로 4개의 실험군으로 나뉘고 4 종류의 서로 다른 레진 시멘트(Variolink II(light-cure), Variolink II(dual-cure), Calibra, Super-Bond C&B)를 이용하여 제조사의 지시에 따라 부착하였다. 부착된 시편은 강도 측정 전에 $37^{\circ}C$ 에서 24시간 동안 생리식염수에 보관하였다. 만능시험기를 사용하여 1mm/min 의 crosshead speed로 각 시편에 힘을 가하여 전단결합강도를 측정하였다. 측정된 결합강도는 SPSS V12.0을 사용하여 일원배치 분산분석으로 비교 분석하였으며, 사후 검증은 Tukey HSD test를 이용하여 분석하였다. Super-Bond C&B의 전단결합강도는 Calibra, Variolink II(light-cure), Variolink II(dual-cure)에 비해 유의하게 낮은 값을 나타내었다(P<.01). Calibra, Variolink II(light-cure), Variolink II(dual-cure)는 전단결합강도에서 서로 유의한 차이를 보이지 않았다. 광중합형과 이원 중합형 레진 시멘트의 전단결합강도는 자가 중합형 시멘트보다 높았다.

• 한국산학기술학회논문지
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• 제21권1호
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• pp.61-69
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• 2020

본 논문은 국내 고속형 화물열차에 적용되는 P4a 분배밸브를 갖는 화물열차의 장대 편성시 제동특성에 관한 것이다. 제동신호가 열차의 끝단까지 연결된 제동관을 통해 공기압력으로 전달되는 화차의 제동은 열차 길이와 사용된 밸브 등에 따라 영향을 받기 때문에 실험적 방법으로 확인한다. 장대화물 열차의 제동 특성은 평상시 운영의 약 2배인 50량으로 구성한 화물열차의 비상제동과 상용제동의 시험을 이용하였다. 1, 10, 20, 30, 50번째 차량에서 제동 실린더 압력이 측정되었다. 열차의 길이가 길어질수록 후방의 차량은 제동이 늦게 체결되는 제동지연 현상을 확인하였으며 특히 비상제동시 차량간 충격이 클 것을 예상할 수 있었다. 제한된 시험의 결과를 보완하고 향후 제동거리 계산을 위해 열차를 구성하는 모든 차량에서의 제동 압력을 예측할 필요가 있다. 제동시 각 차량에서의 압력은 계산시간의 단축과 신뢰성 있는 정보를 제공하는 것으로 알려진 선형보간, 단계형, 지수함수형의 경험적 모델들을 이용하여 예측하였다. 경험적 모델들의 예측결과는 실측한 결과들과 비교하였으며 지수함수형 모델이 비교적 정확하게 예측하고 있음을 확인하였다. 본 연구의 결과는 장대화물열차의 안전한 운용에 기여하고 화물열차의 제동거리 예측과 제동시 차량간 충격량 계산 등에 활용될 수 있을 것으로 예상된다.