• 전자공학회논문지SC
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• 제45권2호
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• pp.37-44
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• 2008

본 논문에서는 고속 링 발진기를 이용한 WLAN용 5.8 GHz PLL을 제안하였다. 제안한 PLL에 사용된 링 발진기는 부 스큐 지연방식을 이용하여 차동 구조로 설계되었다. 따라서 Power-Supply-Injected Noise에 둔감하며, 1/f Noise를 감소시키기 위하여 Tail Current Source를 사용하지 않았다. 제안한 링 발진기는 $0{\sim}1.8V$의 컨트롤 전압에 걸쳐 $5.13{\sim}7.04GHz$의 발진주파수를 보였다. 본 논문에서 제안한 PLL 회로는 0.18 um 1.8 V TSMC CMOS 라이브러리를 기본으로 하여 설계하였고 시뮬레이션을 통하여 성능을 검증하였다. 동작 주파수는 5.8 GHz이며, Locking Time은 2.5 us, 5.8 GHz에서의 소비 전력은 59.9mW로 측정되었다.

• 한국자동차공학회논문집
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• 제6권2호
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• pp.12-20
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• 1998

Exter ballistics of a typical high-speed projectile is studied through a flow-visualization experiment and an unstructured grid Navier-Srokes computation. Experiment produced a schlieren photograph that adequately shows the characteristic features of this complex flow, namely two kinds of oblique cone shocks and turbulent wake developing into the downstream. A hybrid scheme of finite volume-element method is used to simulate the compressible Reynolds-Averaged Navier-Stok- es solution on unstructured grids. Osher's approximate Riemann solver is used to discretize the cinvection term. Higher-order spatial accuracy is obtained by MUSCL extension and van Albada ty- pe flux limiter is used to stabilize the numerical oscillation near the solution discontinuity. Accurate Gakerkin method is used to discretize the viscous term. Explict fourth-order Runge-Kutta method is used for the time-stepping, which simplifies the application of MUSCL extension. A two-layer k-$\varepsilon$ turbulence model is used to simulate the turbulent wakes accurately. Axisymmetric folw and two-dimensional flow with an angle of attack have been computed. Grid-dependency is also checked by carrying out the computation with doubled meshes. 2-D calculation shows that effect of angle of attack on the flow field is negligible. Axi-symmetric results of the computation agrees well with the flow visualization. Primary oblique shock is represented within 2-3 meshes in numerical results, and the varicose mode of the vortex shedding is clearly captured in the turbulent wake region.

• Restorative Dentistry and Endodontics
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• 제9권1호
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• pp.101-106
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• 1983

It was the purpose of this study to investigate the fracture mode of dental amalgam by observing the crack propagation, and to relate this to the microstructure of the amalgam. Caulk 20th Century Regular, Caulk Spherical, Dispersalloy, and Tytin amalgam alloys were used for this study. After each amalgam alloy and Hg measured exactly by the balance was triturated by the mechanical amalgamator (Capmaster, S.S. White), the triturated mass was inserted into the cylindrical metal mold which was 4 mm in diameter and 12 mm in height and was pressed by the Instron Universal Testing Machine at the speed of 1mm/min with 120Kg. The specimen removed from the mold was stored in the room temperature for a week. This specimen was polished with the emery papers from #100 to #200 and finally on the polishing cloth with 0.06${\mu}Al_2O_3$ powder suspended in water. The specimen was placed on the Instron testing machine in the method similar to the diametral tensile test and loaded at the crosshead speed of 0.05mm/min. The load was stopped short of fracture. The cracks on the polished surface of specimen was examined with scanning electron microscope (JSM-35) and analyzed by EPMA (Electron probe microanalyzer). The following results were obtained. 1. In low copper lathe-cut amalgam, the crack went through the voids and ${\gamma}_2$ phase, through the ${\gamma}_1$ phase around the ${\gamma}$ particles. 2. In low copper spherical amalgam, it was observed that the crack passed through the ${\gamma}_2$ and ${\gamma}_1$ phase, and through the boundary between the ${\gamma}_1$ and ${\gamma}$ phase. 3. In high copper dispersant (Dispersalloy) amalgam, the crack was found to propagate at the interface between the ${\gamma}_1$ matrix and reaction ring around the dispersant (Ag-Cu) particles, and to pass through the Ag-Sn particles. 4. In high copper single composition (Tytin) amalgam, the crack went through the ${\gamma}_1$ matrix between ${\eta}$ crystals, and through the unreacted alloy particle (core).

• 한국통신학회논문지
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• 제24권7B호
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• pp.1322-1330
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• 1999

B-ISDN과 같은 초고속 네트워크에서 전송오류의 주요원인은 과잉밀집 상태에 있어서의 버퍼 오버플로우이며 이로 인해 셀 손실을 야기한다. 기존의 통신 프로토콜은 손실된 패킷이나 전송에러들을 다루기 위해 ARQ와 같이 오류회복을 위해 재전송 기법을 사용하고 있으나 이러한 ARQ 방법들은 재전송으로 인한 전송 지연시간이 매우 크기 때문에 초고속 네트워크에서는 적합하지 않다. 따라서 본 논문은 이러한 문제를 줄이기 위하여 B-ISDN에서 FEC를 이용한 셀손실 회복기법을 제안하였다. 제안된 기법은 새로운 순서번호(SN)인 SN*를 이용하여 연속적인 셀손실을 식별한다. SN*는 SN이외에 다른 두 개의 필드(ST, LI)를 조합하여 생성한 순서번호로 그 특성에 따라 가산적(additive) SN*와 승산적(multiplicative) SN*로 구분된다.이러한 연구결과로 FEC는 네트워크 노드상에 버퍼 오버플로우로 인한 셀손실이 발생한 경우에 유용하며 B-ISDN과 같은 초고속 통신망에서의 셀손실 회복에 효과적으로 사용할 수 있는 오류에 기법임을 보여주고 있다. 본 논문에서 제안된 효율적인 셀손실 회복기법은 향후 ATM 네트워크에서의 우선순위 제어, 과잉밀집 제어 등의 연\ulcorner에 효율적으로 사용될 수 있다.

• 대한전자공학회논문지SD
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• 제46권12호
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• pp.30-35
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• 2009

본 논문에서는 3GPP (third generation partnership project) 릴리즈 7 고속 패킷 접속 에볼루션 규격에 포함된 기능 중 기지국 수용 능력 향상, 지연 시간 단축, 그리고 단말소비 전력 감소를 목적으로 새롭게 추가된 연속적인 패킷 연결 프로토콜의 유연한 설계 구조에 대한 것이다. 상기 프로토콜이 3GPP 고속 패킷 접속 규격 기준으로 새롭게 추가된 기능임에 착안하여, 기존 설계 및 검증된 고속 패킷 접속 플랫폼에서 최소한의 하드웨어 변경 및 추가만으로 상기 프로토콜이 구현되도록 고려하였다. 상기 제안된 연속적인 패킷 연결 프로토콜은 비연속적인 송/수신 모드 관련 신호 생성부와 기존 고속 패킷 접속 플랫폼과의 연동을 위한 인터페이스부로 구분된다. 마지막으로 제안된 연속적인 패킷 연결 프로토콜은 셀룰러 이동통신 분야에 적합하도록 규정화된 검증 단계에 따라 기존 고속 패킷 접속 FPGA 단말 모뎀 플랫폼 상에서 다양한 시나리오에 따라 검증되었다.

• International Journal of Aeronautical and Space Sciences
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• 제13권1호
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• pp.117-125
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• 2012

This paper presented the design of SRPS, ground function test, and the deployment test on a high speed taxi of KC-100 airplane. KAI has developed a spin recovery system in collaboration with Airborne Systems for KC-100 general aviation airplane. Spin mode analysis, rotary balance and forced oscillation tests were performed to obtain the rotational, dynamic derivatives in the preliminary design phase. Prior to the detailed design process of SRPS, approximations for initial estimation of design parameters- fineness ratio, parachute porosity, parachute canopy filling time, and deployment method- were considered. They were done based on the analytical disciplines such as aerodynamics, structures, and stability & control. SRPS consists of parachute, tractor rocket assembly for deployment, attach release mechanism (ARM) and cockpit control system. Before the installation of SRPS in KC-100 airplane, all the control functions of this system were demonstrated by using SBTB(System Breakout Test Box) in the laboratory. SBTB was used to confirm if it can detect faults, and simulate the firing of pyrotechnic devices that control the deployment and jettison of SRPS. Once confirmed normal operation of SRPS, deployment and jettison of parachute on the high speed taxiing were performed.

• 대기
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• 제28권4호
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• pp.469-477
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• 2018

We performed the comparison of observed $PM_{10}$ and $PM_{2.5}$ at both the Yonsei University and the AIRKOREA site in the same Seodaemun-gu district, Seoul from March to December 2016. Generally, the moderate correlations between two sites were found for both $PM_{10}$ and $PM_{2.5}$, but monthly difference was somewhat occurred, implying that the measurement situation is not equally maintained even in a closely located area. Particularly correlations became weaker in June and July, which seems the impact of rainy conditions. Correlations between two stations were higher for $PM_{10}$ compared to $PM_{2.5}$, probably indicating the spatially larger difference of fine mode particle. Monthly mean variation was similar between two sites showing a maximum in March and minimum in August. Diurnal variation was somewhat different: morning peak at Yonsei University but evening peak at the Seodaemun-gu AIRKOREA site, reflecting the difference of local air condition. We also compared the extent of $PM_{10}$ and $PM_{2.5}$ according to the local wind speed and direction. In general, the level of particulate matter was high when the wind is blowing from the northwestern area with low wind speed, meaning the high accumulation effect of transported air particles. Findings of this study can be usefully considered for the investigation about the discrepancy of aerosol measurement in a local scale.

• Wind and Structures
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• 제34권2호
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• pp.185-197
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• 2022

This study aimed to analyze the wind-induced mechanical energy (WME) of a proposed super high-rise and long-span transmission tower-line system (SHLTTS), which, in 2021, is the tallest tower-line system with the longest span. Anew index - the WME, accounting for the wind-induced vibration behavior of the whole system rather than the local part, was first proposed. The occurrence of the maximum WME for a transmission tower, with or without conductors, under synoptic winds, was analyzed, and the corresponding formulae were derived based on stochastic vibration theory. Some calculation data, such as the drag coefficient, dynamic parameters, windshielding areas, mass, calculation point coordinates, mode shape and influence function, derived from wind tunnel testing on reducedscale models and finite element software were used in calculating the maximum WME of the transmission tower under three cases. Then, the influence of conductors, wind speed, gradient wind height and wind yaw angle on WME components and the energy transfer relationship between substructures (transmission tower and conductor) were analyzed. The study showed that the presence of conductors increases the WME of transmission towers and changes the proportion of the mean component (MC), background component (BC) and resonant component (RC) for WME; The RC of WME is more susceptible to the wind speed change. Affected by the gradient wind height, the WME components decrease. With the RC decreasing the fastest and the MC decreasing the slowest; The WME reaches the its maximum value at the wind yaw angle of 30°. Due to the influence of three factors, namely: the long span of the conductors, the gradient wind height and the complex geometrical profile, it is important that the tower-line coupling effect, the potential for fatigue damage and the most unfavorable wind yaw angle should be given particular attention in the wind-resistant design of SHLTTSs

• 한국지반공학회논문집
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• 제30권7호
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• pp.5-15
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• 2014

휴 폐광산지는 산발생, 지하수 오염뿐만 아니라 침식 및 산사태 등 다양한 물리화학적 지질재해에 노출되어 있다. 임기광산 폐석적치장 광미를 대상으로 링 전단시험을 수행하여 전단속도에 따른 전단특성을 조사하고 한다. 본 연구에 있어 마찰저항을 최소화할 목적으로 링 전단상자 오링(O-ring)은 전단동안 회전이 가능하도록 설계되었다. 1차 시험은 일정한 수직응력(50kPa)과 전단속도(0.1mm/sec) 조건에서 전단시간에 따른 전단응력을 조사하였다. 2차 시험은 일정한 수직응력 조건에서 전단속도를 0.01, 0.1, 1, 10, 50, 100mm/sec로 순차적으로 증가시켜 전단속도에 따른 전단응력을 조사하였다. 3차 시험은 일정한 전단속도(0.1mm/sec)하에서 수직응력을 20, 40, 60, 80, 100, 150kPa로 증가시켜 각 경우에 대한 전단응력을 조사하였다. 시험결과에 따르면, 배수조건에 관계없이 임기광산 폐석적치장광미시료는 전단연화거동(strain softening behavior)을 보였다. 특히 전단속도가 10mm/sec보다 작은 경우 잔류전단응력은 100~300초 사이에 일정한 값에 도달하는 것으로 나타났다. 2차와 3차 시험결과에 따르면, 배수조건에 관계없이 전단응력은 전단속도와 수직응력의 함수로 나타났다. 하지만, 배수조건에 따라 링 전단상자 전단부에서 상이한 입자파쇄 특성이 관측되었다. 배수조건시 전단상자 전단면에서 하단까지 넓은 전단띠가 형성된 것에 반해, 비배수조건시 전단면에 국부 전단띠가 형성되었다. 이러한 점에 비추어 볼 때, 전단속도에 따른 입자파쇄 특성은 산사태 유동성을 높이는 중요한 인자로 판단된다.

• Tribology and Lubricants
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• 제36권2호
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• pp.105-115
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• 2020

This paper presents a numerical study on the rotordynamic analysis of a dual-spool turbofan engine in the context of blade defect events. The blades of an axial-type aeroengine are typically well aligned during the compressor and turbine stages. However, they are sometimes exposed to damage, partially or entirely, for several operational reasons, such as cracks due to foreign objects, burns from the combustion gas, and corrosion due to oxygen in the air. Herein, we designed a dual-spool rotor using the commercial 3D modeling software CATIA to simulate blade defects in the turbofan engine. We utilized the rotordynamic parameters to create two finite element Euler-Bernoulli beam models connected by means of an inter-rotor bearing. We then applied the unbalanced forces induced by the mass eccentricities of the blades to the following selected scenarios: 1) fully balanced, 2) crack in the low-pressure compressor (LPC) and high pressure compressor (HPC), 3) burn on the high-pressure turbine (HPT) and low pressure compressor, 4) corrosion of the LPC, and 5) corrosion of the HPC. Additionally, we obtained the transient and steady-state responses of the overall rotor nodes using the Runge-Kutta numerical integration method, and employed model reduction techniques such as component mode synthesis to enhance the computational efficiency of the process. The simulation results indicate that the high-vibration status of the rotor commences beyond 10,000 rpm, which is identified as the first critical speed of the lower speed rotor. Moreover, we monitored the unbalanced stages near the inter-rotor bearing, which prominently influences the overall rotordynamic status, and the corrosion of the HPC to prevent further instability. The high-speed range operation (>13,000 rpm) coupled with HPC/HPT blade defects possibly presents a rotor-case contact problem that can lead to catastrophic failure.