• Journal of Radiation Protection and Research
• /
• 제27권3호
• /
• pp.171-179
• /
• 2002

대기 중으로 방출된 방사성물질의 이동 확산 현상을 이해하기 위하여 3차원 장거리 확산 모델이 개발되었다. 모델은 수평방향으로 방출점으로부터 수천 키로 미터의 거리까지 공기중 농도와 지표면 침적을 계산하도록 설계되었다. 수직 난류운동은 혼합층 내와 혼합층 위로 분리하도록 고려하였다. 시험계산은 동북 아시아권의 영역을 고려하였고, 방출점은 중국의 동쪽 지점을 가정하였다. 계산된 농도분포는 바람장에 의해 방출점의 남동방향을 향해 주로 이동되었다. 개발된 모델은 원전 사고시 방사선 피해를 추정하기 위하여 이용될 것이며, 모델은 장거리 야외확산실험의 자료를 이용하여 비교 검증 연구를 통하여 보완될 것이다.

• 한국지구과학회지
• /
• 제41권4호
• /
• pp.323-343
• /
• 2020

Observation data measured at Ieodo Ocean Research Station (IORS) have been utilized in oceanographic and atmospheric studies since 2003. Sea level data observed at the IORS have not been paid attention as compared with many other variables such as aerosol, radiation, turbulent flux, wind, wave, fog, temperature, and salinity. Total sea level rises at the IORS (5.6 mm yr^-1) from both satellite and tide-gauge observations were higher than those in the northeast Asian marginal seas (5.4 mm yr^-1) and the world (4.6 mm yr^-1) from satellite observation from 2009 to 2018. The rates of thermosteric, halosteric, and steric sea level rises were 2.7-4.8, -0.7-2.6, 2.3-7.4 mm yr^-1 from four different calculating methods using observations. The rising rate of the steric sea level was higher than that of the total sea level in the case with additional data quality control. Calculating the non-steric sea level was not found to yield meaningful results, despite the ability to calculate non-steric sea level by simply subtracting the steric sea level from total sea level. This uncertainty did not arise from the data analysis but from a lack of good data, even though tide, temperature, and salinity data were quality controlled two times by Korea Hydrographic and Oceanography Agency. The status of the IORS data suggests that the maintenance management of observation systems, equipment, and data quality control should be improved to facilitate data use from the IORS.

• Wind and Structures
• /
• 제29권1호
• /
• pp.75-84
• /
• 2019

A steady slot suction near the free-end leading edge of a finite-length square cylinder was used to control its aerodynamic forces and vortex-induced vibration (VIV). The freestream oncoming flow velocity ($U_{\infty}$) was from 3.8 m/s to 12.8 m/s. The width of the tested cylinder d = 40 mm and aspect ratio H/d = 5, where H was the height of the cylinder. The corresponding Reynolds number was from 10,400 to 35,000. The tested suction ratio Q, defined as the ratio of suction velocity ($U_s$) at the slot over the oncoming flow velocity at which the strongest VIV occurs ($U_{\nu}$), ranged from 0 to 3. It was found that the free-end slot suction can effectively attenuate the VIV of a cantilevered square cylinder. In the experiments, the RMS value of the VIV amplitude reduced quickly with Q increasing from 0 to 1, then kept approximately constant for $Q{\geq}1$. The maximum reduction of the VIV occurs at Q = 1, with the vibration amplitude reduced by 92%, relative to the uncontrolled case. Moreover, the overall fluctuation lift of the finite-length square cylinder was also suppressed with the maximum reduction of 87%, which occurred at Q = 1. It was interesting to discover that the free-end shear flow was sensitive to the slot suction near the leading edge. The turbulent kinetic energy (TKE) of the flow over the free end was the highest at Q = 1, which may result in the strongest mixing between the high momentum free-end shear flow and the near wake.

• Wind and Structures
• /
• 제28권5호
• /
• pp.285-298
• /
• 2019

For super long-span bridges, the aerodynamic forces induced by the flow passing the box girder should be considered carefully. And the Reynolds number sensitively of aerodynamic characteristics is one of considerable issue. In the study, a numerical study on the Reynolds number sensitivity of aerodynamic characteristic (flow pattern, pressure distribution and aerodynamic forces) of a twin-box girder were carried out using large eddy simulation (LES) with the dynamic Smagorinsky-Lilly subgrid model. The results show that the aerodynamic characteristics have strong correlation with the Reynolds number. At the leading edge, the flow experiences attachment, departure, and reattachment stages accompanying by the laminar transition into turbulence, causing pressure plateaus to form on the surface, and the pressure plateaus gradually shrinks. Around the gap, attributing that the flow experiences stages of laminar cavity flow, the wake with alternate shedding vortices, and turbulent cavity flow in sequence with an increase in the Reynolds number, the pressures around the gap vary greatly with the Reynold number. At the trailing edge, the pressure gradually recovers as the flow transits to turbulence (the flow undergoes wake instability, shear layer transition-reattachment station), In addition, at relative high Reynolds numbers, the drag force almost does not change, however, the lift force coefficient gradually decreases with an increase in Reynolds number.

• 대기
• /
• 제34권2호
• /
• pp.153-176
• /
• 2024

At 0843 UTC 30 May 2021, a commercial aircraft encountered severe turbulence at z = 11.5 km associated with the rapid development of Mesoscale Convective System (MCS) in the Gyeonggi Bay of Korea. To investigate the generation mechanisms of Near-Cloud Turbulence (NCT) near the MCS, Weather Research and Forecasting model was used to reproduce key features at multiple-scales with four nested domains (the finest ∆x = 0.2 km) and 112 hybrid vertical layers. Simulated subgrid-scale turbulent kinetic energy (SGS TKE) was located in three different regions of the MCS. First, the simulated NCT with non-zero SGS TKE at z = 11.5 km at 0835 UTC was collocated with the reported NCT. Cloud-induced flow deformation and entrainment process on the downstream of the overshooting top triggered convective instability and subsequent SGS TKE. Second, at z = 16.5 km at 0820 UTC, the localized SGS TKE was found 4 km above the overshooting cloud top. It was attributed to breaking down of vertically propagating convectively-induced gravity wave at background critical level. Lastly, SGS TKE was simulated at z = 11.5 km at 0930 UTC during the dissipating stage of MCS. Upper-level anticyclonic outflow of MCS intensified the environmental westerlies, developing strong vertical wind shear on the northeastern quadrant of the dissipating MCS. Three different generation mechanisms suggest the avoidance guidance for the possible NCT events near the entire period of the MCS in the heavy air traffic area around Incheon International Airport in Korea.

• 대한기계학회논문집
• /
• 제16권11호
• /
• pp.2150-2158
• /
• 1992

본 연구에서는 복잡한 유동형태를 지닌 충돌분사류에 대한 유동특성을 연구하 기 위하여 단순화된 실험모델로써 형상이 동일한 두 원형분류의 충돌에 의한 충돌분류 의 혼합현상 및 유동구조 등을 질량유량비의 변화에 따라 유체역학적으로 구명하고자 하였으며, 본 연구 결과는 연소기관에서의 연소효율 증대 및 구조개선등의 공학적 응 용을 위한 기본자료로 활용하고, 이론적 연구에 의한 난류의 유동구조 및 유동특성 에 대한 타당성 입증과 이론적 모델의 보완을 위한 실험자료로 이용하고자 한다. 충돌유동에 영향을 미치는 주요인자는 노즐직경, 충돌각, 충돌질량유량비, 온도, 밀도 등이며, 이 인자들 중에서 충돌질량유량비와 출돌각이 충돌후 형성되는 난류혼합유동 에 지배적인 영향을 미치므로, 본 연구에서는 두 원형분류의 충돌질량유량비를 가변할 수 있는 장치를 고안하였으며, 두 분류의 충돌각을 45˚로 고정하고, 고속측과 저속측 노즐의 질량유량비를 1.0, 0.8, 0.6, 0.4로 설정하여 질량유량비에 따른 혼합 유동구 조의 구명을 위한 실험적인 연구를 수행하였다. 충돌후의 혼합유동의 특성을 연구하 기 위하여 유동중심궤적, 유동반폭, 유동단면, 2차원 및 3차원 유동장, 평균속도분포 등을 온라인 컴퓨터시스템을 이용하여 측정분석하였다.

• 한국수산과학회지
• /
• 제17권2호
• /
• pp.83-91
• /
• 1984

$1982{\sim}83$년과 $1966{\sim}70$년의 해양관측자료를 사용하여 하계 우리나라 서해 연안에서 형성되는 조석전선의 형성원인과 그 위치 및 구조를 조사하였다. 하계에 형성되는 전선은 조류에 의한 해저 난류로 연직혼합이 일어나는 곳과 외해와의 경계성이며, 그 위치는 수온, 염분, 용존산소의 수평경도와 수색 및 투명도로써 조사한 결과, G선($35^{\circ}31^'N$)과 S선($35^{\circ}25^'N$)의 연안에서 약 20mile 떨어진 해역이었다. 성층상태를 고려한 위치에너지는 V=10 $Joule/m^3$였으며, 수온, 염분, 용존산소와 수색 및 투명도로 조사한 전선의 위치는 이와 대체로 일치하였다. 따라서 이 역을 경계로 연안쪽은 물리, 화학적인 특성이 연직적으로 균일한 혼합층을 형성한다. 외해쪽에는 수면에서 약 $10{\sim}20m$까지 표면 혼합층, 약층, 그리고 저층 혼합층의 순으로 수괴의 구조가 형성되 어 있다. 동계에는 서해 전역이 표면냉각으로 인하여 전 해역에서 연직혼합이 일어나므로 하계의 구조와 같은 전선은 명확하게 형성되지 않는다.