• 대한기계학회논문집B
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• 제23권5호
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• pp.661-669
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• 1999

The evolutionary structure of a tip vortex in the initial period have been investigated by the two-dimensional LDV system. Circumferential and axial components of mean velocities, their turbulences and Reynolds stresses were measured by the phase averaging technique at seven different wake ages within one revolution of the rotor. Core growth was also analyzed. It was resulted that circumferential velocity components showed a Rankine combined vortex shape and their circulation profiles viewed in the radial direction were close to the n = 2 model of Vatistas' algebraic formula, while axial velocity components seemed to have the Gaussian profiles In these measured ranges with the base width of three times of core radii. Peaks of circumferential velocities and core radii showed distinct asymmetric behaviors before the wake age of $150^{\circ}$ over inboard and outboard sides of the slipstream, but they became symmetric afterwards. Turbulence profiles which had two peaks Inside the core radii in the earlier wake age were also changed to single peaks after $150^{\circ}$. These trends imply that the tip vortex was barely mature at this wake age.

• 한국항공우주학회지
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• 제44권3호
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• pp.212-217
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• 2016

저궤도 위성용 S대역 수신기 EM 모델을 개발 하였다. 복조기는 복조 방식의 확장성을 고려하여 복조 기능을 FPGA를 사용하여 구현하였으며 제작된 수신기는 RF 단과 디지털 복조기 그리고 전원부로 구성되고 운용상 발생되는 주파수 편이 보상을 위한 도플러 추적 기능을 가진다. 측정결과 수신기의 BER은 -110dBm의 RF입력전력에서 $1.0{\times}10^{-6}$로 측정 되었으며, 중심 주파수를 기준으로 ${\pm}100KHz$의 주파수 추적기능을 가진다. 요구된 환경 온도 테스트를 완료하였으며, TID 테스트 결과 기준치인 10Krad를 만족한다.

• 한국연소학회지
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• 제3권2호
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• pp.13-27
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• 1998

The optimization of frontal device including fuel nozzle and swirler is required to secure the mixing of fuel and air and the combustion stability leading the reduction of pollutant emissions and the increase of combustion efficiency in gas turbine combustor. The effects of injection nozzle and swirler on the flow field, spray characteristics and consequently the combustion stability, were experimentally investigated by measuring the velocity field, droplet sizes of fuel spray, lean combustion limit and the temperature field in the main combustion region. Flow fields and spray characteristics were measured with APV(Adaptive Phase Doppler Velocimetry) under atmospheric condition using kerosine fuel. Temperatures were measured by Pt-Pt13%Rh, R-type thermocouple which was 0.2mm thick. Spray and flame was visualized by ICCD(Intensified Charge Coupled Device) camera. It was found that the dual swirler resulted in the biggest recirculation zone with the highest reverse flow velocity at the central region, which lead the most stable combustion. The various combustion characteristics were observed as a function of the geometries of injector and swirler, that gave a tip for the better design of gas turbine combustor.

• 한국측량학회지
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• 제30권6_2호
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• pp.607-613
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• 2012

Ionospheric anomaly is one of the major error sources which deteriorate the GNSS performance. In the equatorial region, effects of the ionospheric plasma bubbles are of great interest because they are pretty common phenomena, especially in the period of the high solar activity. In order to evaluate the GNSS performance under circumstance of the bubbles, an ionospheric scintillation monitor has been developed and installed in Bangkok, Thailand. Furthermore, a model simulating the ionospheric delay and scintillation due to the bubbles has been developed. Based on these developments, the effects of the simulated plasma bubbles are analyzed and their agreement with the real observation is demonstrated. An availability degradation of the GPS ground based augmentation system (GBAS) caused by the bubbles is exampled in details. Finally, an integrated GPS/INS approach based on the Doppler frequency is proposed to remedy the deterioration.

• 천문학회보
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• 제36권2호
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• pp.97.2-97.2
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• 2011

Rims of solar filaments often appear brighter than the background chromosphere, but their physical nature is still poorly known. Last year, we observed a filament with a bright rim. The rim was bright in H alpha but not in Ca II 8542 line. Using the cloud model, we inferred physical parameters of the region from the spectral profiles. As a result, we found that the Doppler width of the H alpha line is very large, which implies temperature as high as 50000K. In addition, the value of the source function of the H alpha line is 0.7 times the continuum intensity of background profile. These results suggest that the bright rims might be a region of intense heating, probably associated with a current sheet. To further investigate this possibility, we carried out more observations this summer. We will present new results obtained from the analysis of these observations and discuss the physical implication of these measurements on the nature of bright rims and the filaments.

• 한국연소학회:학술대회논문집
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• 한국연소학회 1998년도 제17회 KOSCI SYMPOSIUM 논문집
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• pp.9-21
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• 1998

The optimization of frontal device including fuel nozzle and swirler is required to secure the mixing of fuel and air, and the combustion stability in the gas turbine combustor design for the reduction of pollutant emissions and the increase of combustion efficiency. The effects of injection nozzle and swirler on the flow field, spray characteristics and consequently the combustion stability, were experimentally investigated by measuring the velocity field, droplet sizes of fuel spray, lean combustion limit and the temperature field in the main combustion region. The effect of fuel injection nozzle was tested by adopting three different nozzles; a dual orifice fuel nozzle, a hollow cone nozzle and a solid cone nozzle. These tests were combined with the three different swirler geometries; a dual-stage swirler with 40$^{\circ}$ /-4 5$^{\circ}$ vanes and two single-stage swirlers with 40$^{\circ}$ vane angle having 12 and 16vanes, respectively. Flow fields and spray characteristics were measured with APV(Adaptive Phase Doppler Velocimetry) under atmospheric condition using kerosine fuel. Temperatures were measured by Pt-PtI3%Rh, R-type thermocouple which was 0.2mm thick. It was found that the dual swirler resulted in the biggest recirculation zone with the highest reverse flow velocity at the central region, which lead the most stable combustion. The various combustion characteristics were observed as a function of the combination between the injector and swirler, that gave a tip for the better design of gas turbine combustor.

• International Journal of Fluid Machinery and Systems
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• 제4권1호
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• pp.150-160
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• 2011

This study focuses on the Achard turbine, a vertical axis, cross-flow, marine current turbine module. Similar modules can be superposed to form towers. A marine or river hydropower farm consists of a cluster of barges, each gathering several parallel rows of towers, running in stabilized current. Two-dimensional numerical modelling is performed in a horizontal cross-section of all towers, using FLUENT and COMSOL Multiphysics. Numerical models validation with experimental results is performed through the velocity distribution, depicted by Acoustic Doppler Velocimetry, in the wake of the middle turbine within a farm model. As long as the numerical flow in the wake fits the experiments, the numerical results for the power coefficient (turbine efficiency) are trustworthy. The overall farm efficiency, with respect to the spatial arrangement of the towers, was depicted by 2D modelling of the unsteady flow inside the farm, using COMSOL Multiphysics. Rows of overlapping parallel towers ensure the increase of global efficiency of the farm.

• 한국통신학회논문지
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• 제36권8B호
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• pp.1021-1027
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• 2011

해상에서는 지상에서와 같은 고속의 통신 수단이 존재하지 않으며 주로 초단파를 이용하여 기본적인 정보나 음성 통신을 수행하고 있다. 지상의 경우 이론적인 해석 결과나 실험 결과를 바탕으로 하는 통신 채널 모델이 존재하나 해상의 경우에는 제한적인 연구 결과가 존재하고 있는 실정이다. 본 논문에서는 초단파 영역의 해상 채널 특성 파악을 위하여 지상에 송신국을 설치하고 선박에 수신국을 설치하여 거리에 따른 해상 채널 특성을 살펴보았다. 해석 결과에 따르면 선박의 이동에 의한 도플러 변이가 관측되며 거리가 증가함에 따라 에너지가 감소하고 있으며 특히 수직/수평 또는 수평/수직 채널에 대하여 통계적인 특성이 크게 변화하고 있는 결과를 가지고 있음을 알 수 있다.

• Nuclear Engineering and Technology
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• 제18권2호
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• pp.71-77
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• 1986

원자로 노심을 축방향으로 일차원 해석을 하고, 가입경수로형원자로의 안전성 해석에 적용할 수 있는 중성자 동특성프로그램 BIK를 개발하였다. BIK프로그램내에서 공간변수에 대해서는 유한차분법이, 시간변수에 대해서는 $\theta$-시간적분법이 채택되었다. 또한 도플러 및 감속재 궤환과 제어봉구동 등을 자세히 묘사하는 모델들이 포함되었다 핵모델의 검증은 ANL검증문제를 통해 이루어졌고, 고리 1호기의 제어봉 인출사고시의 노심출력 변화를 계산하였다. 이상의 계산결과 BIK동특성프로그램이 노심의 중성자 속 변화를 일차원해석의 한계내에서 비교적 정착하게 묘사할 수 있으며, 가압경수로형 원자로의 안전성 해석에 유용하게 사용될 수 있다는 것이 증명되었다.

• 대한전자공학회논문지TC
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• 제46권3호
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• pp.19-25
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• 2009

본 논문에서는 이동통신채널에서 발생하는 간섭현상을 제거하기 위한 적응형 채널추정(adaptive channel estimate) 알고리듬을 제안하였다. 기존 LMS 알고리듬은 입출력사이 오차를 줄이기 위해 사용하는 첫 기준신호의 선택에 따라 수렴속도와 오차정확도에 많은 영향을 받는다. 본 논문에서 제안한 적응형 채널추정 알고리듬은 간섭신호와 유사한 기준신호를 정하기 위해 LMS 알고리듬을 수행하기 전에 병렬의 컨볼루션 연산을 수행한다 컨볼루션 연산을 통해 출력된 신호는 채널의 지연시간과 진폭특성을 가지고 있어 간섭신호와 유사한 특성을 가진다. 제안된 알고리듬의 성능평가는 이동통신환경과 유사한 Jake's 모델에 Doppler 주파수는 130 Hz, Random한 5개의 경로가 존재하는 Rayliegh 다중경로 채널환경에서 실험하였다. 모의실험결과 기존 LMS 알고리듬은 데이터 150개를 반복 수행함으로써 약 -40 dB의 제곱오차수렴을 보였고 제안한 적응형 채널추정 알고리듬은 데이터 200개를 반복 수행함으로써 약 -80 dB의 제곱오차수렴을 보였다. 데이터의 반복연산에 따른 수렴속도는 다소 증가하였으나 제곱오차정확도는 약 40 dB의 우수한 개선특성을 보였다.