• 한국측량학회:학술대회논문집
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• 한국측량학회 2004년도 추계학술발표회 논문집
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• pp.295-301
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• 2004

Satellite captures images periodically and economically over the area wider than aerial photographs, and reconnaissance to unapproachable area. For these advantages, mapping using high resolution satellite image has high potentials of marketability and development. Therefore, utilization of satellite image in mapping and GIS is expected to be growing and research on describable feature, positional accuracy and, possible mapping scale is urgently needed. This research presented that Quick Bird orthoimage could be used to update digital map on a scale of 1:5,000. Quick Bird image was corrected geometrically based on ground control points. DEM was generated using height data of digital topographic map. The orthoimge was produced by digital differential rectification based on DEM which was generated using height data of digital topographic map(scale 1;5,000 and 1;1,000). When the digital topographic map was overlaid with the orthoimage, it was very easy to find changed region or new features builded after the map compiled.

• 한국연소학회지
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• 제5권2호
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• pp.63-68
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• 2000

Combustion phenomenon in scale-downed combustor is investigated. As the combustor scale decreases surface to volume ratio increases and chamber size approaches quenching distance. As the combustor scales down surface to volume ratio increases resulting increased heat loss. And this heat loss can affect quenching and instability of the flame. To investigate this effect plastic mini combustor is made. Stoichiometricaly premixed Hydrogen / air gas is used as fuel. Initial chamber pressure and chamber size are varied and the effects are evaluated. Peak pressure decreased with the decrease in chamber height. As initial chamber pressure decreases peak pressure decreases and this change is more important than scale down effect till the chamber height of 1mm. With this result and further information following the experiments design parameter for micro engine can be established.

• International Journal of Fluid Machinery and Systems
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• 제2권4호
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• pp.353-362
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• 2009

In the process of turbine modernizations, the investigation of the influences of water passage roughness on radial flow machine performance is crucial and validates the efficiency step up between reduced scale model and prototype. This study presents the specific losses per component of a Francis turbine, which are estimated by CFD simulation. Simulations are performed for different water passage surface roughness heights, which represents the equivalent sand grain roughness height. As a result, the boundary layer logarithmic velocity profile still exists for rough walls, but moves closer to the wall. Consequently, the wall friction depends not only on roughness height but also on its shape and distribution. The specific losses are determined by CFD numerical simulations for each component of the prototype, taking into account its own specific sand grain roughness height. The model efficiency step up between reduced scale model and prototype value is finally computed by the assessment of specific losses on prototype and by evaluating specific losses for a reduced scale model with smooth walls. Furthermore, surveys of rough walls of each component were performed during the geometry recovery on the prototype and comparisons are made with experimental data from the EPFL Laboratory for Hydraulic Machines reduced scale model measurements. This study underlines that if rough walls are considered, the CFD approach estimates well the local friction loss coefficient. It is clear that by considering sand grain roughness heights in CFD simulations, its forms a significant part of the global performance estimation. The availability of the efficiency field measurements provides an unique opportunity to assess the CFD method in view of a systematic approach for turbine modernization step up evaluation. Moreover, this paper states that CFD is a very promising tool for future evaluation of turbine performance transposition from the scale model to the prototype.

• 한국가스학회지
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• 제21권5호
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• pp.56-63
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• 2017

전세계적으로 수소 충전 스테이션 구축에 많은 투자와 지원을 하고 있는 실정이다. 그러나 수소는 폭발범위가 넓고 확산이 빠른 기체이다. 본 연구에서는 액화수소를 취급하는 소규모~대규모 충전스테이션을 대상으로, 사고시 발생하는 VCE로 인한 피해영향범위를 산출하고, 프로빗 모델을 통해 주변의 인적, 물적 피해를 예측하였다. 더불어, 벤트스택 끝단에서 발생 가능한 Jet fire를 시나리오로 선정하여 최적 높이를 설정하였다. 피해영향범위는 관심과압 6.9kPa을 기준으로 하여, 소규모 저장시설의 경우 8.24m, 중규모 14.10m, 대규모 22.38m이다. 폐출혈로 인한 인체 피해는 소규모와 중규모가 각각 50m, 대규모 100m였으며, 구조물 손상에 따른 피해는 소규모 200m, 중규모 300m 및 대규모 500m이다. 벤트스택의 최적높이는 소규모 4.7m, 중규모 8.8m 및 대규모 16.9m이다.

• 한국대기환경학회지
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• 제16권2호
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• pp.141-150
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• 2000

In order to genralize the vertical dispersion of plume at long distances on mesoscale over complex terrain dispersion coefficients data have been obtained systematically according to lapsed time after release by using a composite turbulence water tank that simulates convective boundary layer. Dispersion experiments have been carried out for various combined conditions of thermal turbulence intensity mechanical turbulence intensity and plume release height at slightly to moderately unstable conditions. Results of tracer dispersion experiments conducted using water tank camera and image processing system have been converted into atmospheric dispersion data through the application of similarity law. The equation $\sigma$z/Zi=aX/(b+c X2)0.5 where $\sigma$2; vertical dispersion coefficient zi : mixing height X : dimen-sionaless downwind distance was confirmed to be an appropriate and general equation for expressing $\sigma$2 variation with turbulence intensity and plume release height, The value of "a" was found to be principally affected by mechanical turbulence intensity and that of "b" by mechanical turbulence intensity and release height. It was confirmed that the magnitude of "c" varies with release height. Results of water tank experiments on the relationship of $\sigma$2 vs downwind distance x have been compared with actual atmospheric dispersion data such as CONDORS data and Bowne's nomogram Operating conditions of a composite turbulence water tank for simulating the field turbulence situations of CONDORS experiments and Bowne's $\sigma$2(x) nomogram for suburban area have also been investigated in terms of water temperature difference between convection water tank and bottom plate heating tank grid plate stroke mixing water depth length scale and velocity scale. Moreover the effect of mechanical turbulence intensity on vertical dispersion has been discussed in the light of release height and downwind distance. height and downwind distance.

• 대한원격탐사학회지
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• 제36권2_2호
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• pp.325-335
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• 2020

식생 높이는 높이-탄소식생량 추정 모델을 이용하여 식생탄소량은 측정하는데 사용된다. 접근이 힘든 지역의 망그로브 생태는 현장 자료를 취득하는데 어려움이 있으며, 제한적인 현장 자료로부터 대규모 식생량 및 탄소양모델을 연구하는데 한계점이 있다. 능동형과 수동형 원격탐사 기법이 망그로브 식생 연구에 활용되고 있으나, 공간 해상도의 한계로 인해 작은 규모의 특징을 감지하는데 문제가 있다. 이 논문에서는 TanDEM-X 자료를 이용하여 SRF 지역 12 m 공간 해상도 망그로브 식생 높이 분포를 측정하였다. 단일 편파를 사용하였지만, 수면과 망그로브 식생 사이에서 일어나는 이중 반사 현상을 이용하여 망그로브 숲 지역의 수면의 높이를 측정하여 식생 높이를 측정하는 새로운 인버젼 모델을 사용하였다. TanDEM-X 식생 높이 결과를 모자이크하여 SRF 전 지역의 대규모 식생 높이 지도를 제작하였다. 현장 자료와 검증한 결과 상관계수 0.83, RMSE 0.84 m로 나타났다. 전 세계를 관측한 TanDEM-X 자료를 이용하면, 고해상도 글로벌 망그로브 식생 높이 지도 제작이 가능함을 보여주었다. 이러한 결과들은 망그로브 식생탄소량 및 탄소 순환을 이해하는데 중요한 역할을 할것으로 기대된다.

• 천문학회지
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• 제29권spc1호
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• pp.69-70
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• 1996

• 한국산학기술학회논문지
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• 제19권5호
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• pp.1-8
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• 2018

본 연구는 Siphon Breaker Simulation Program(SBSP)을 이용하여 소규모 사이펀 차단기 실험장치를 설계 및 제작하고, 실험 수행 후 그 결과를 이용하여 다양한 규모의 사이펀 차단기에 대한 SBSP의 적용 가능성을 평가하기 위해 진행되었다. 실험장치 설계를 위하여 C factor와 Chisholm B 계수, Undershooting Height(UH)에 대한 시뮬레이션 결과값을 SBSP로 도출하였다. 실험장치의 중요파트는 upper tank, lower tank, downcomer, Siphon Breaker Line(SBL) 등이며, upper tank는 넓이 $0.09-m^2$, 높이 0.65-m의 크기로 제작되었고, downcomer 높이는 1.6-m로 제작되었다. 실험결과 분석을 위하여 압력계, 차압계, 전자저울이 사용되어 압력과 차압, 유량에 대한 정보를 도출하였다. 실험에서 사용된 실험변수는 Loss Of Coolant Accident(LOCA) 크기와 SBL 크기이며, LOCA는 30-mm와 38-mm에 대해서, SBL은 6/16-inch와 8/16-inch에 대해서 실험이 진행되었다. 실험의 결과로 유량과 압력, 그리고 UH를 도출하였으며, 실험결과를 SBSP의 시뮬레이션 결과와 비교, 분석하였다. UH 측면에서 SBSP가 수조의 총 높이 대비 2.5 %의 오차로 실험결과를 잘 예측하는 것을 관찰하였다. 그러므로 SBSP를 이용한 다양한 규모의 사이펀 차단기 설계가 가능한 것을 확인하였다.

• 대한원격탐사학회:학술대회논문집
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• 대한원격탐사학회 2008년도 International Symposium on Remote Sensing
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• pp.344-347
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• 2008

Ocean surface waves may be modified by ocean current and their observation may be severely distorted if the observer is on a moving platform with changing speed. Tidal current near a sill varies inversely with the water depth, and results spatially inhomogeneous modulation on the surface waves near the sill. For waves propagating upstream, they will encounter stronger current before reaching the sill, and therefore, they will shorten their wavelength with frequency unchanged, increase its amplitude, and it may break if the wave height is larger than 1/7 of the wavelength. These small scale (${\sim}$ 1 km changes is not suitable for satellite radar observation. Spatial distribution of wave-height spectra S(x, y) can not be acquired from wave gauges that are designed for collecting 2-D wave spectra at fixed locations, nor from satellite radar image which is more suitable for observing long swells. Optical images collected from cameras on-board a ship, over high-ground, or onboard an unmanned auto-piloting vehicle (UAV) may have pixel size that is small enough to resolve decimeter-scale short gravity waves. If diffuse sky light is the only source of lighting and it is uniform in camera-viewing directions, then the image intensity is proportional to the surface reflectance R(x, y) of diffuse light, and R is directly related to the surface slope. The slope spectrum and wave-height spectra S(x, y) may then be derived from R(x, y). The results are compared with the in situ measurement of wave spectra over Keelung Sill from a research vessel. The application of this method is for analysis and interpretation of satellite images on studies of current and wave interaction that often require fine scale information of wave-height spectra S(x, y) that changes dynamically with time and space.

• 한국산학기술학회논문지
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• 제16권10호
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• pp.7138-7145
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• 2015

본 연구에서는 KS C 9306에 따른 난방 제상능력 시험조건(건구온도 $2^{\circ}C$/습구온도 $1^{\circ}C$)에서 확대모형이 아닌 실제 열교환기의 전방에 디지탈 현미경과 광센서의 발광부와 수광부를 나란히 설치하여 광센서 출력전압과 서리 높이간의 연관성을 규명하기 위한 실험을 수행하였다. 150개의 실험 데이터로부터 서리높이를 예측할 수 있는 선형 상관식을 개발하여 계산한 결과, 측정값의 54%가 상관식으로 예측한 값의 ${\pm}10%$ 이내에서 일치하였으며 서리 높이가 0.3mm 이상의 실험데이터에서는 데이터의 90% 이상이 ${\pm}10%$ 이내에서 일치하였다. Xiao 등의 상관식과 비교하였을 때 출력전압 변화에 따른 서리 높이의 변화를 나타내는 기울기는 2.3% 오차 범위에서 일치하였으나 Xiao 등의 상관식은 실제 열교환기가 아닌 모사 열교환기를 사용한 이상적인 조건에서 개발되었기 때문에 절편 값에서는 큰 차이를 보였다.