• Proceedings of the Korean Vacuum Society Conference
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• 2013.02a
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• pp.649-649
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• 2013

그래핀은 우수한 전기적, 광학적, 기계적인 특성들로 인해 주목을 받아왔지만 그래핀의 상용화에는 많은 문제점들이 있었다. 그 중 비교적 고품질의 대면적 그래핀 필름을 얻기 위한 방법으로 화학증기 증착법이 개발됨에 따라 그래핀 합성은 더 이상 어려운 문제는 아니다. 다만, 소자 제작에 있어서 좋은 전하이동도와 저항을 유지하기 위해 소자 제작과정 중의 도핑의 감소가 중요하다. 본 연구에서는 화학증기 증착법을 통해 만들어진 그래핀 소자 제작과정 중 그래핀 전사과정에서의 도핑을 줄이기 위한 방법으로 전기화학적 박리법(버블링 전사)을 이용하였고 이 때 사용되는 전해질의 종류에 따라 도핑의 영향을 분석하였다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.33 no.9
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• pp.1-8
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• 2005

This paper explored the effects of separation control through the use of pulsating jet blowing on a two dimensional elliptical airfoil. To develop an active control technique of flow separation, a flow control actuator utilizing continuous/pulsed jet of pressurized air was designed and installed in a wind tunnel testing model of elliptic wing. PIV measurement and flow visualization of the wing near field were conducted to access the feasibility and effectiveness of the pulsed jet blowing on controlling the stall of the elliptical wing in subsonic flow. PIV experimental results show that separation control can provide significant reduction in turbulent flow wake and separation bubbles by jet blowing. The pulsating jet blowing is more effective on the separation control than continuous one. Increased jet frequency suppressed the turbulent separated flow wake effectively at even higher AOAs.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.37 no.1
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• pp.69-75
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• 2009

This paper studies the aerodynamic performance that the vent mixer-new conceptual supersonic mixer-showed with its geometric characteristics. The hole is 2 mm with 2 mm's distance from the wall in case 1 and with no distance in case 2. In case 3 die hole is 1 mm. Case 1 and case 2 showed the same total pressure recovery ratio, of which the case 3 was lower than that. While cases 1-3 had the same reattachment length, the shear layer was thicker in cases 1 and 2 than in case 3. Within the recirculation zone, cases 1 and 2 had lower pressure loss and higher velocity gradient difference than case 3-they enhance mixing between air and fuel. Separation bubble which is developed by the inflow into the recirculation zone has a significant effect on the total pressure recovery ratio in the combustor. Also separation bubble influences pressure distributions and recirculation flows in the recirculation zone. Therefore, inflow rate of air into the recirculation zone mainly affects the performance of vent mixer.

• Journal of Korean Society of Steel Construction
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• v.20 no.6
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• pp.751-759
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• 2008

In this study, the effect of an unsteady flow field around a body of aerostatic/aerodynamic forces were investigated using rectangular cylinders (B/D = 2, 3, 4, 5). Proper orthogonal decomposition (POD) was introduced to the analysis of the fluctuating pressure field that was measured on the stationary/oscillatory B/D=4 rectangular cylinder, and the characteristics of the proper functions with flow patterns were identified. In addition, the physical decoupling and interactions in the different co-existing flow patterns were investigated through POD. The comparison with the identified proper function associated with a particular flow pattern revealed that the Karman vortex is almost not affected by the separation bubble, but that the Karman vortex considerably interferes in the development of the separation bubble around the trailing edge. It can be considered that the Karman vortex induces the increment of the curvature of the substantial separated flow.

• 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.

• Korean Journal of Air-Conditioning and Refrigeration Engineering
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• v.13 no.11
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• pp.1134-1140
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• 2001

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 dimension. Power law scheme and SIMPLE algorithm were used for convective diffusion formulation and pressure term respectively. Governing equations were discretized by control volume formulation. The flow patterns and heat transfer were predicted in details. The convective heat transfer coefficients were affected by separation bubbles which appeared at the wake region of offset strip fins.

• Transactions of the Korean Society of Mechanical Engineers B
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• v.39 no.10
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• pp.795-803
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• 2015

The boundary layer developing over the suction surface of a first-stage turbine blade for power generation has been investigated in this study. For three locations selected in the region where local thermal load changes dramatically, mean velocity, turbulence intensity, and one-dimensional energy spectrum are measured with a hot-wire anemometer. The results show that the suction-surface boundary layer suffers a transition from a laminar flow to a turbulent one. This transition is confirmed to be a "separated-flow transition", which usually occurs in the shear layer over a separation bubble. The local minimum thermal load on the suction surface is found at the initiation point of the transition, whereas the local maximum thermal load is observed at the location of very high near-wall turbulence intensity after the transition process. Frequency characteristics of turbulent kinetic energy before and after the transition are understood clearly from the energy spectrum data.

• Proceedings of the Korean Vacuum Society Conference
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• 2014.02a
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• pp.385.2-385.2
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• 2014

그래핀은 전기적, 광학적, 역학적, 열적 특성 등이 아주 좋은 소재이다. Thermal Chemical Vapor Deposition (T-CVD) 장비를 이용 저 진공, 고온에서 CH4과 H2를 가스를 사용하여 그래핀을 합성을 하였다. 그래핀은 탄소만으로 이루어진 2차원 층상구조를 가지고 있다. 촉매 금속 위에서 합성이 이루어지기에 합성된 그래핀을 바로 다른 응용하기에는 어려움이 따른다. 따라서 촉매 금속에서 그래핀을 분리하여 원하는 곳으로 옮기는 과정이 필요한데, 이를 전사공정이라 한다. 최근 전기분해를 이용하여 발생되는 수소 버블을 사용하여 그래핀을 촉매로 사용되는 금속으로부터 분리해내는 Electrochemical Delamination(ED) 전사방식이 소개가 되었다. 이러한 전사 방식의 장점은 촉매기판을 제거하지 않음으로써, 다시 재활용이 가능하고, 공정에 필요한 시간이 짧다. 또한 표면에서 직접적으로 분리하는 방식이기에 촉매 금속의 양면을 사용이 가능하다. 이러한 ED방식의 장점이 있기에 공정의 최적 조건을 잡기 위하여 변수들을 바꾸어가면서 실험을 하였다. 전사된 그래핀은 표면을 광학현미경으로 확인하였고, 라만 분광기를 사용하여 라만 스펙트럼과 기본적인 전기특성을 확인하여 특성을 평가하면서, 기존의 전사방식을 사용한 그래핀 샘플과 비교분석 하였다.

• Journal of the Korea Institute of Military Science and Technology
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• v.6 no.4
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• pp.29-37
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• 2003

Using a wind tunnel testing, the aerodynamic load characteristics of an elliptic airfoil was described. The experimental data was obtained for angles of attack $-20^{\circ}$ to $+20^{\circ}$ with $2^{\circ}$ increments at a chord Reynolds number of $0.99{\times}105$ and $2.48{\times}105$. For each test case, chordwise suction pressure distributions and wake surveys were obtained. Static pressure measurements were made over a 10 sec averaging time at a 10 Hz sampling rate. For each case, wake survey was conducted with a pilot-static probe at 1.0c downstream from the trailing edge at very fine spacing to resolve the wake velocity deficit profile. As can be expected, suction pressure coefficient was increased with angle of attack. The normal force, CNmax, appeared peak value at the incidence angle of $12^{\circ}~14^{\circ}$, and the significant increase in profile drag at this range of angles of attack.