• 항공우주기술
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• 제9권1호
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• pp.17-27
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• 2010

알루미나 입자가 포함된 KSLV-I KM 고공 플룸 유동을 연소실에서 노즐 출구의 고공 팽창과정을 해석하였다. 알루미나 입자 및 플룸 가스의 물성치 및 분포를 달리하여 해석한 결과 연소가스 비열비를 1.2로 알루미나 입자의 직경 분포를 7가지로 가정하면 노즐 내부 유동 특성이 평형유동 해석 결과와 비교적 일치하였다. 입자의 팽창각은 가스유동보다 작으며 입자 직경이 클수록 팽창각은 더 작았다. 알루미나 입자의 광학 열물성을 변화시키며 KM TVC 분배기 위치의 복사열을 계산한 결과 알루미나 입자의 방사율이 0.1일 때 비행시험 결과와 비슷한 수준을 예측하였다.

• 대한원격탐사학회:학술대회논문집
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• 대한원격탐사학회 2003년도 Proceedings of ACRS 2003 ISRS
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• pp.869-872
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• 2003

The thermal contamination of the Younggwang coastal marine ecosystem has been investigated using space borne thermal infrared data acquired over the period 1985-2003 by the Landsat and NOAA satellites. The analysis of AVHRR data brought out the general pattern and extension of thermal plume while TM data yielded more accurate information about the plume shape, dimension, dispersion direction etc. The examination of sea surface temperature (SST) computed from these images clearly indicates that the thermal plume extends 70 to100km southward during summer and 50 to70km northwestward during winter monsoons. The maximum plume temperature was 29$^{\circ}C$ in summer and 12$^{\circ}C$ in winter. The comparative analysis shows that the temperature retrieved from TM is slightly higher (1.8$^{\circ}C$, 3$^{\circ}C$ and 2.2$^{\circ}C$ for the images of 98/11/10, 99/05/05 and 99/05/21 respectively) than those derived from AVHRR data. The correlation coefficient between the TM-derived SST and AVHRR-derived SST was 0.72.

• Wind and Structures
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• 제27권6호
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• pp.417-430
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• 2018

The concentration fields in the proximities of a local gas emission source are experimentally analyzed in several combinations of wind incidences and source emissions. These conditions are determined by the plume buoyancy, emission velocity and incident flow wind speed. Concentration measurements are performed by an aspirating probe in a boundary layer wind tunnel. The analysis included the mean concentration values and the intensity of concentration fluctuations in a neutral atmospheric boundary layer flow. Different configurations are tested: an isolated stack in a homogeneous terrain and a stack with a bluff body in close proximity, located windward and leeward from the emission source. The experimental mean concentration values are contrasted with Gaussian profiles and the dilution factor is analyzed with respect to the empirical curves of the minimum dilution. Finally, a study on the plume intermittency is performed in a cross-sectional plane near the emission source. It is possible to highlight the following observations: a) plume vertical asymmetry in the case of an isolated emission source, b) significant differences in the dispersion process related to the relative location of the emission source and bluff body effects, and c) different probabilistic behavior of the concentration fluctuation data in a cross-sectional measurement plane inside the plume.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2011년 춘계학술대회논문집
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• pp.601-604
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• 2011

Plume flow-fields of aircraft nozzles are numerically investigated at various flight conditions for infrared signature analysis. A mission profile of subsonic unmanned combat aerial vehicle is considered for the requirement of each mission, associated engine and nozzles are selected through a performance analysis. Numerical results of nozzle plume flow-fields using a CFD code are analyzed in terms of thrust, maximum temperature. It is shown that maximum temperature increase for lower altitude and higher Mach number.

• 한국전산유체공학회지
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• 제16권3호
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• pp.15-21
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• 2011

Aerothermodynamic flowfields of aircraft engine nozzles are computationally investigated at various flight conditions for infrared signature analysis. A mission profile of subsonic unmanned combat aerial vehicle is considered for the case study and associated engine and nozzles are selected through a performance analysis. Computational results of nozzle and plume flowfields using a density-based CFD code are analyzed in terms of thrust, maximum temperature, length and optical thickness of plume. It is shown that maximum temperature, length, and optical thickness of nozzle plume increase for lower altitude and higher Mach number.

• 환경영향평가
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• 제2권1호
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• pp.57-63
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• 1993

An analysis for particle settling effects via of plume centerline tilted exponentially under the influence of panicle settling velocity is carried out for particle of $30{\mu}m$ diameter with $1g/cm^3$ density and 0.02m/s settling velocity corresponding to its particle characteristic according to various wind speeds, atmospheric stabilities. Characteristic analysis of surface concentration distribution simulated by Lagrangian model also are carried out under the influence of plume centerline tilted exponentially at 10m stack height emitted 200 particles per second. This study reveals that plume centerline at the nearby source is sharply tilted exponentially under the condition of stable, weakly wind speed, therefore the lower concentration at the nearby source, the higher concentration at the downwind distance far away from source than actual one is brought out, if not apply the effect of plume centerline tilted exponentially to diffusion Model.

• Nuclear Engineering and Technology
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• 제17권3호
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• pp.216-223
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• 1985

원자력 발전소로부터 방출되는 기체상 방사성 물질에 의한 환경 영향을 평가함에 있어서 방사성 물질의 대기중에서의 수송과 확산을 기술하는 모델로써 Gaussian plume mode띠 널리 사용되고 있다. Gaussian plume model은 평탄한 지형에 적용하도록 만들어진 모델이므로 대부분의 국토가 복잡한 산악으로 구성된 한극의 경우에 적용하기 위해서는 모델의 수정이 필요하다. 본 논문에서는 2차원적 x-ｚ 평면에서 확산방정식을 해석한 numerical diffusion model과 Gaussian plume model을 비교하여, Gaussian plume mode에서 가장 중요한 변수인 dispersion coefficient를 지형의 높이에 대하여 보정하였다. 보정된 dispersion coefficient 값을 Gaussian plume mode에 적용시켜 계산을 수행한 결과를 보면, 산악지역에서의 방사성 물질의 농도는 평지에서보다 낮게 나타나고 있다.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2008년도 춘계학술대회논문집
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• pp.440-443
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• 2008

Plume radiation has been measured during ground tests of KSLV-I kick motor in order to predict the thermal load on the equipment around the kick motor at flight. The measuring positions are the kick motor base, and the measured heats were about 2${\sim}$5 w/cm$^2$. The measured heat showed a lot of shot fluctuation in their values, and the radiative heats at the latter half of time are higher than those of the first half. A plausible explanation for these phenomena was given as the variation of alumina particles with time. The radiative heats along the plume axis were also measured recently at 8 positions with 1.5m radius from plume axis, but only the initial parts of the results could be acceptable because the sensor were damaged by the accumulated heat. The strongest heat occurred at the middle of the plume, which can be explained with different view factors. Despite of the plausible explanation, it seems to need more analysis because the plume structure such as temperature, alumina particle, after burning has not been revealed until yet. The measure heat flux has been reflected in the prediction of the plume radiation at high altitude where the kick motor operates.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2004년도 제22회 춘계학술대회논문집
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• pp.479-484
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• 2004

Reactions of NO$_{x}$, HO$_{x}$ and $O_3$ chemistry in a diffusion process of the exhaust plume under a stratospheric condition were investigated numerically. Expanding Box method was used to assess the effects of exhaust gases from a stratospheric flight system on $O_3$ depletions. Sensitivity analysis was also performed to identify prime reactions of $O_3$ depletions in an exhaust plume right after the nozzle. In addition, a calculation of reactive flows in stratospheric condition was performed to investigate the characteristics of reactions in a plume. As a result of this study, prime reactions of NO$_{x}$, HO$_{x}$ and $O_3$chemistry in an exhaust plume were identified, and fundamental behavior of chemical species were examined in a exhaust plume.t plume.

• 한국추진공학회지
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• 제6권1호
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• pp.12-20
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• 2002

케로신/액체산소 추진기관을 갖는 KSR-III 로켓의 플룸 유동장에 대하여 로켓 동체/플룸 유동장에 대한 통합적인 해석을 수행하였다. 기체 열-화학 모델이 유동장에 미치는 영향을 평가하여 로켓 유동장을 해석하는 목적에 가장 적합한 기체 모델을 제시하기 위하여 열량적 완전기체, 다윈 화학종 반응기체, 그리고 화학적 동결기체의 세 가지 기체 모델을 사용하여 유동장을 해석하고 그 차이를 검토하였다. 반응유동 해석 결과는 노즐 내부에서의 화학반응에 의한 연소가스의 온도 증가로 인해 다른 기체 열화학 모델에 비해 전체적으로 더 높은 온도 분포를 나타내었다. 플룸에서의 모든 화학반응은 전단류와 배럴 충격파 반사지점 후방의 고온 영역에 국한되어 일어났으며, 본 해석의 경우 플룸 내에서의 유한속도 화학반응이 유동에 미치는 영향은 미약한 것으로 나타났다. 그러나 본 연구에서 이루어진 유한속도 화학반응을 고려한 플룸 해석을 통하여 플룸에서의 주된 화학반응 및 반응 메커니즘을 확인할 수 있었다.