• Title/Summary/Keyword: Gas Dispersion

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A Study on the Consequences of Underground High Pressure Natural Gas Pipelines (고압 매몰 천연가스 배관 누출사고 피해해석에 관한 연구)

  • Lee, Seungkuk;Shin, Hun Yong
    • Journal of the Korean Institute of Gas
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    • v.17 no.2
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    • pp.44-49
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    • 2013
  • Due to rapid rise of consuming rate for natural gas, installation and operation of high pressure natural gas pipeline is inevitable for high rate of gas transportation. Accordingly incidents on the underground high pressure natural gas pipeline come from various reasons will lead to massive release of natural gas and gas dispersion in the air. Further, fire and explosion from ignition of released gas may cause large damage. This study is for release rate, dispersion and flash fire of natural gas to establish a safety management system, setting emergency plan and safety distance.

Revealing ionized gas kinematics at the center of nearby Seyfert galaxies

  • Kim, Eun Chong;Woo, Jong-Hak
    • The Bulletin of The Korean Astronomical Society
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    • v.39 no.1
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    • pp.43.2-43.2
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    • 2014
  • We investigate the ionized gas kinematics at the center of 6 nearby Seyfert galaxies, using the integral field spectroscopy data from the Calar Alto Legacy Integral Field spectroscopy Area survey Data Release 1. To understand the kinematic nature of the ionized gas in the narrow-line regions (NLRs), we measured the flux, velocity, and velocity dispersion of the [OIII] $5007{\AA}$ and Ha $6563{\AA}$ emission lines, after subtracting a best-fit stellar population model representing the stellar features. At the same time, we measured stellar velocity as a reference for the systemic velocity, and stellar velocity dispersion. We spatially resolved the velocity structure of the ionized gas using each emission line and compared it to that of stars. In this poster we present the flux, velocity, and velocity dispersion maps of the ionized gas and stars, and discuss the nature of the ionized gas outflows in the central kiloparsec scale.

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Diffusion and Disperision of Injected $CO_2$Gas Into the $N_2$Gas Flow ($N_2$기체의 흐름에 주입된 $CO_2$기체의 확산 및 분산)

  • 김유식;안대영
    • Fire Science and Engineering
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    • v.16 no.3
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    • pp.1-7
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    • 2002
  • Diffusion and dispersion of injected $CO_2$gas into the $N_2$ gas flow are complex. In the packed column with porous particles the axial dispersion and the extra-particle mass transport as well as the intra-particle mass transport are involved. The pulse spreads by stationary diffusion during the period of arrested flow. Hence, the effect of axial dispersion, and of entrance and exit, as well as that of intraparticle convection should be eliminated during the period. The effective diffusivity was determined experimentally by using the gas chromatography, which is to arrest the gas flow during the period after injecting the pulse. This experiment method hasn't been used often in the field. Effective diffusivities are raised with temperature increasing, and it is quite satisfied com-pared to literature values. In this study, the calculated data of gaseous chemical for extinguish fires could be helpful to appreciate several physical phenomenons. Also, it could be expected that, the calculated data of this study might be very useful for development of excellent gaseous chemical for extinguish fires and improvement of its efficiency.

Effect of gas composition on dispersion characteristics of blowout gas on offshore platform

  • Yang, Dongdong;Chen, Guoming;Shi, Jihao;Li, Xinhong
    • International Journal of Naval Architecture and Ocean Engineering
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    • v.11 no.2
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    • pp.914-922
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    • 2019
  • Gas composition has a significant impact on the dispersion behavior and accumulation characteristics of blowout gas. However, few public studies has investigated the corresponding effect of gas composition. Therefore, this study firstly builds the FLACS-based numerical model about an offshore drilling platform. Then several scenarios by varying the composition of blowout gas are simulated while the scenario with the composition of "Deepwater Horizon" accident is regarded as the benchmark. Furthermore, the effects of the gas composition on the flammable cloud volume, the influenced area of flammable cloud, the influenced area of hydrogen sulfide and the critical time of the hydrogen sulfide spreading to the living area are analyzed. The results demonstrate that gas composition is a driving factor for dispersion characteristics of blowout gas. All the results can give support to reduce the risk of the similar accidents incurred by real blowouts.

Exreaction of Thiosulfinates from Garlic Using Gas-in-Liquid-Dispersion

  • Lee, Won-Yiong;Bae, Dong-Ho;Park, Yong-Hee
    • Preventive Nutrition and Food Science
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    • v.1 no.2
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    • pp.179-185
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    • 1996
  • Extraction yields of thiosulfinates from garlic were studied by using gas-in-liquis-dispersion(GLD) system to maxmize the thiosulfinate extraction. Extracted thiosulfinates were spectrophotometically quantified using synthesized dially1 thiosulfinate. The conditions for maximum extraction were optimized by response surface methodology. The volatile components extracted by various methods, such as hexane extraction, simultaneous steam distillation and GLD system, were compared by using gas chromatography. The results indicated that the thiosulfinate yield was increased by incresaing temperature and nitrogen gas flow rate, while the effects of bubble sizes on thiosulfinate extraction were not significant at the ranges tested. Application of GLD system resulted in extraction of more volatile components than other extraction methods, Therfore, it was suggested that GLD system was one of the efficient extraction methods among the ever introduced ones, for thiosulfinate extraciton.

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A Study on the Dispersion of Hydrogen Gas in Atmosphere (대기 중 수소가스의 확산거동에 관한 연구)

  • Ahn Bum Jong;Jo Young-Do
    • Journal of the Korean Institute of Gas
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    • v.9 no.1 s.26
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    • pp.9-15
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    • 2005
  • Hydrogen is considered to be the most important future energy carrier in many applications reducing significantly greenhouse gas emissions, but the safety issues associated with hydrogen applications need to be investigated and fully understood to be applicable as the carrier. Therefore, there is a considerable demand for further research concerning the dispersion of hydrogen/air mixture clouds and the possible consequences of their ignition. In this study, the dispersion of hydrogen gas in atmosphere has been analysed with atmospheric condition by concerning the buoyancy of hydrogen. The hazard ranges to wind direction increase with wind speed and the stability of atmosphere. The concentration of hydrogen at just above ground is nearly zero due to buoyancy of hydrogen gas. Therefore, the ignition probability of hydrogen gas cloud is low and the hazard of explosion or fire associated with hydrogen gas is relatively low comparing with the other fuel gas such as propane or butane.

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Performance Dispersion Analysis and Applications of Gas Generator Cycle Liquid Rocket Engine (가스발생기 사이클 액체 로켓 엔진의 성능 분산 해석 및 활용)

  • Nam, Chang-Ho;Cho, Won-Kook;Seol, Woo-Seok
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2006.11a
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    • pp.191-195
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    • 2006
  • It is definitely required to control dispersion of the rocket engine performance in order to accomplish the mission of a launch vehicle successfully. A performance dispersion analysis was conducted for a gas generator cycle liquid rocket engine and the required pressure drops were estimated for engine tunning. As a result, the vacuum thrust dispersion of the engine was from +9.1% to -8.7% and the mixture ratio deviated from +9.7% to -9.6% from the nominal value due to the errors of components and the engine inlet condition of propellants. The required pressure drop in the LOx line to the combustor is higher than in the fuel line for same mixture ratio change.

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Performance Dispersion Analysis of Gas Generator Cycle Liquid Rocket Engine (가스발생기 사이클 액체 로켓 엔진의 성능 분산 해석)

  • Choi Hwan Seok;Nam Chang Ho
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2004.10a
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    • pp.87-91
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    • 2004
  • It is definitely required to control dispersion of the rocket engine performance in order to accomplish the mission of launch vehicle successfully. We performed the dispersion analysis of gas generator cycle LRE (liquid rocket engine) accompanied with ANASYN. As a result, the vacuum thrust dispersion of the engine was $+5.34\%,\;-5.27\%$ and the mixture ratio deviated $+9.07\%,\;-9.82\%$ from the nominal value due to the errors of components and engine inlet condition of propellants. By applying the gas generator regulator only, the dispersion of the engine performance increases. Error in turbine efficiency is the most influential factor to the dispersion of engine performance.

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Simulation Study of NOx Dispersion from Power Plant Stack Gas (화력발전소 배출가스 중 질소산화물의 확산에 관한 연구)

  • Park, Mi-Jeong;Jo, Young-Min;Sung, Doo-Yong;Kim, Mi-Jeong;Park, Young-Koo
    • Journal of the Korean Applied Science and Technology
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    • v.30 no.3
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    • pp.540-550
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    • 2013
  • Various efforts have been explored to save the cost in many industrial fields. In order to recover the residual thermal energy from the flue gas, an extreme high efficiency heat exchanger is planning to install at a power plant. The gas temperature will be reduced to $40^{\circ}C$ from $115^{\circ}C$. Thus gas buoyancy decreases, and dispersion of nitrogen oxides is expected to deteriorate as increasing relative humidity. In this study, the conversion of nitrogen monoxide to nitrogen dioxide and dispersion regime are investigated through computational modeling. Nitrogen dioxide which indicates 0.1 ppm at 85 m from the ground could be propagated to 620 m at $115^{\circ}C$ of the flue gas, whilst when cooled down to $40^{\circ}C$, it expands up to 750 m. The ground level influence area showed more expansion of dispersion, approximately to 930 m.

A Study on Dispersion Analysis and Calibration of Gas Generator Cycle Liquid Rocket Engine (가스발생기 사이클 액체로켓엔진의 성능분산해석과 엔진성능보정)

  • Nam, Chang-Ho;Kim, Seung-Han;Kim, Cheul-Woong;Seol, Woo-Seok
    • Aerospace Engineering and Technology
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    • v.6 no.1
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    • pp.120-127
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    • 2007
  • Performance dispersion in the engine should be considered to predict the flight accuracy of a launch vehicle. A dispersion estimation method was presented with a LOx/Kerosene gas generator cycle engine. The orifices in the propellant supply lines in the engine were assumed to be used for calibration of the performance and the required pressure drops were acquired. The dispersions after calibration were quantified also.

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