• Proceedings of the Korean Information Science Society Conference
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• 2004.04a
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• pp.928-930
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• 2004

명령어간의 데이터 종속 관계는 동적으로 스케줄 되는 파이프라인 프로세서의 병렬 처리에 중요한 장애로 남아 있다. 마이크로프로세서의 데이터 종속에 기인한 파이프라인 대기 시간을 줄일 대표적인 두 가지 방법으로 생성 값의 지역성에 기초를 둔 데이터 값 예측과 공간 지역성에 기반으로 예측하는 주소 예측이 있다. 본 논문에서는 성능 개선을 위해 이 두 가지 기술을 독립적으로 수행하는 것 보다 혼합한 형태의 예측이 더 좋은 예측 정확성이 나타나는 것을 보인다.

• The Journal of Korean Institute of Electromagnetic Engineering and Science
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• v.14 no.9
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• pp.919-923
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• 2003

In this paper, a double-sided planar balun using Microstrip-to-CPW coupled structure is fabricated and measured. The measured amplitude and phase imbalance are, respectively, less than 0.2 dB and 2.1$^{\circ}$ in a wide frequency range from 2.44 GHz to 4.33 GHz. It is expected that the proposed balun can improved the performance of balanced mixer, amplifier and feeding network of antennas. Also, it can be used in many microwave multilayer structures due to its structural characteristics.

• Proceedings of the KSME Conference
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• 2007.05b
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• pp.1900-1905
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• 2007

A micro cyclone combustor was developed to be used as a heat source of thermoelectric power generator (TPG). The cyclone combustor was designed so that fuel and air were supplied to the combustion chamber separately. The mixing and flow characteristics in the combustor were investigated numerically. The global equivalence ratio (${\Phi}$), defined using the fuel and air flow rates, was introduced to examine the flow features of the combustor. The mixing of fuel and air inside the combustor could be well understood using the fuel concentration distribution. It was found that the weak recirculating zone was formed upper the fuel-supplying tube in case of ${\Phi}$ < 1.0. In addition, it was found that small regions that have a negative axial velocity exist near the fuel injection ports. It is assumed that these negative axial velocity regions can stabilize a flame inside the micro cyclone combustor.

• Proceedings of the KSME Conference
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• 2001.11b
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• pp.155-160
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• 2001

The low NOx characteristics have been investigated to develop the combustor for micro turbine. The lean premixed combustion technology was applied to reduce the NOx emission. The test was conducted at the condition of high temperature and ambient pressure. The combustion air which has the temperature of $450\sim650K$ were supplied to the combustor through the air preheater. The temperature and emissions of NOx and CO were measured at the exit of combustor, The exit temperature and NOx were increased and CO was decreased with increasing inlet air temperature. The premixing chamber can be operated very lean condition of equivalence ratio around 0.35. The NOx was decreased with decreasing the equivalence ratio. The CO was decreased with decreasing the equivalence ratio, but the CO was increased with decreasing the equivalence ratio below 0.4. But, at the very lean condition of equivalence ratio below 0.35 both NOx and CO were increased because of the flame unstability. The NOx was decreased and CO was increased with increasing inlet air flowrate. This results can be used to determine the size of combustor. Consequently the performance of combustor shows the possibility of the application to the gas turbine system.

• Transactions of the Korean Society of Mechanical Engineers B
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• v.31 no.12
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• pp.1042-1047
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• 2007

A micro cyclone combustor was developed to be used as a heat source of thermoelectric power generator (TPG). The cyclone combustor was designed so that fuel and air were supplied to the combustion chamber separately. The mixing and flow characteristics in the combustor were investigated numerically. The global equivalence ratio ($\Phi$), defined using the fuel and air flow rates, was introduced to examine the flow features of the combustor. The mixing of fuel and air inside the combustor could be well understood using the fuel concentration distribution. It was found that the weak recirculating zone was formed upper the fuel-supplying tube in case of ${\Phi}$<1.0. In addition, it was found that small regions that have a negative axial velocity exist near the fuel injection ports. It is assumed that these negative axial velocity regions can stabilize a flame inside the micro cyclone combustor.

• Korean Journal of Air-Conditioning and Refrigeration Engineering
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• v.27 no.2
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• pp.75-80
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• 2015

The effect of inlet mixer geometries on the two-phase flow patterns in square micro-channel with $600{\times}600{\mu}m$ was investigated experimentally in this paper. The 4 different mixer configurations based on the Y, Impacting, and two T types (gas and liquid inlets were switched) were used. The test fluids were nitrogen and water. The liquid and gas superficial velocities were 0.01~10 m/s and 0.1~100 m/s, respectively. Several distinctive flow patterns, namely, annular, slug-annular, slug, slug-bubbly, bubbly, and churn flow could be seen. The flow pattern maps for each mixer were suggested, and it can be concluded that two-phase flow patterns are not very sensitive to the mixer geometries. But the mixing behaviors of gas and liquid for each mixer were different for slug and bubbly flow. Thus, the characteristics of slug and bubble for each case were not same.

• The Journal of Korean Institute of Electromagnetic Engineering and Science
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• v.16 no.7 s.98
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• pp.753-759
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• 2005

In this paper, we have developed a new type of single balanced mixer with the RF MEMS $180^{\circ}$ hybrid coupler using surface micromachining technology. The $180^{\circ}$ hybrid coupler in this mixer is composed of the dielectric-supported air gapped microstriplines(DAMLs) which have signal line with $10{\mu}m$ height to reduce substrate dielectric loss and dielectric posts with size of $20{\mu}m{\times}20{\mu}m$ to elevate the signal line on air with stability At LO power of 7.2 dBm, the conversion loss was 15.5 dB f3r RF frequency or 57 GHz and RF power of -15 dBm. Also, we obtained the good RF to LO isolation of -40 dB at LO frequency of 58 GHz and LO power of 7.2 dBm. The main advantage of this type of mixer is that we are able to reduce the size of the chips due to integrating the MEMS passive components.

• Proceedings of the Korean Vacuum Society Conference
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• 2013.02a
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• pp.374-375
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• 2013

Al/Ni 나노 멀티 포일은 상온에서 외부 방전 및 촉발에 따라 급속한 자기 발열 반응이 일어나는 특성을 보여, 외부 촉발을 통해 상온에서 온도를 높일 수 없는 접합이나 마이크로 수준의 미세 접합이 가능한 접합재료로서 활용이 상당히 기대되는 재료이다. 본 연구에서는 스퍼터링법을 이용하여 한 층이 20 nm 이하에서 Al과 Ni의 혼합 기준을 달리한 Al/Ni 나노 멀티 900층을 제조와 제조된 반응성 포일이 자기 발열 반응에 따른 미세구조에 대해 조사하였다. 박막의 증착은 3~10 mTorr의 공정압력 으로 Al 타겟 전류 1.7 A, Ni 타겟 전류 1.4 A로 하여 증착시간을 조절하여 제조하였다. SEM과 EDX를 통하여 Al/Ni 나노 멀티 포일의 성장구조와 각 원소의 함량을 조사하였다. XRD 미세결정구조 분석은 제조된 반응성 포일과 외부 촉발시킨 후 자기 발열 반응에 의해 형성되는 혼합 상에 대한 조사를 실시하였다. 혼합기준이 1:1의 Al/Ni 나노 멀티 포일에서 약 $980^{\circ}C$의 발열이 발생하는 것을 Pyrometer를 통해 측정하였으며, 자기 발열 반응 후의 혼합 상은 AlNi이 형성되었다. Ni rich 포일에서는 약 $730^{\circ}C$의 발열이 발생하였고, 혼합상으로 주로 AlNi이 형성되었고 Al3Ni2도 나타났으며, 반응에 참여하지 못한 Ni이 남아있는 것을 관찰하였다. Al rich 포일에서는 약 $720^{\circ}C$의 발열과 함께 AlNi, $AlNi_3$이 형성되었고 반응에 참여하지 못한 Al이 미세하게 나타났다.

• Membrane Journal
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• v.22 no.2
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• pp.120-127
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• 2012

In this study, separation of ethylbenzene from mixed xylene was performed by using TS-1 zeolite membrane. TS-1 zeolite membranes were prepared by microwave synthesis and changing the reaction temperature. MFI-type TS-1 membranes are synthesized on alumina tubes by functional coating using 3-chloropropyltrimethoxysilane (3CP-TMS). On top surface of interlayer, nano TS-1 crystals were seeded. To form interlayer, microwave-assisted growth of TS-1 zeolite was carried out and thin zeolite layers were produced. All of the prepared membranes are tested to separate ethylbenzene from mixed xylene at different operating temperatures. TS-1 membrane with zeolite seed synthesized at $170^{\circ}C$ compared to 120, $140^{\circ}C$ shows the best ethylbenzene separation at the operation temperature of $200^{\circ}C$ from ternary mixed xylene containing certain composition of ethylbenzene/p-xylene/m-xylene. (separation factor : 2.64, ethylbenzene flux : 1703.0 mol/$m^2{\cdot}s{\cdot}Pa$).

• Transactions of the Korean Society of Mechanical Engineers B
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• v.37 no.2
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• pp.103-109
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• 2013

In this study, we performed a numerical study of hydrogen/air combustion in the combustion chamber of an ultra micro gas turbine. The supply flow rate and equivalence ratio are used as variables, and the commercial computational fluid dynamic program (STAR-CCM) is used for the numerical study of the combustion. The flow rate significantly affects the flame position, flame temperature, and pressure ratio between the inlet and the outlet. The flame position is close to the outlet in the combustion chamber, and the flame temperature and pressure ratio monotonously increases with the supply flow rate. The change in the equivalence ratio does not affect the flame position. The maximum flame temperature occurs under stoichiometric conditions.