• Title/Summary/Keyword: Plume Model

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Recovery of water and contaminants from cooling tower plume

  • Macedonio, Francesca;Frappa, Mirko;Brunetti, Adele;Barbieri, Giuseppe;Drioli, Enrico
    • Environmental Engineering Research
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    • v.25 no.2
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    • pp.222-229
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    • 2020
  • Membrane assisted condenser is an innovative membrane operation that exploits the hydrophobic nature of microporous membranes to promote water vapor condensation and recovery. It can be used for water and chemicals recovery from waste gaseous streams. In this work, the testing of membrane condenser for water and ammonia recovery from synthetic streams (i.e., a saturated air stream with ammonia) simulating the plume of cooling tower is illustrated. The modeling of the process was carried out for predicting the membrane-based process performance and for identifying the minimum operating conditions for effectively recovering liquid water. The experimental data were compared with the results achieved through the simulations showing good agreement and confirming the validity of the model. It was found that the recovery of water can be increased growing the temperature difference between the plume and the membrane module (DT), the relative humidity of the plume (RHplume) and the feed flow rate on membrane area ratio. Moreover, the concentration of NH3 in the recovered liquid water increased with the growing DT, at increasing NH3 concentration in the fed gaseous stream and at growing relative humidity of the feed.

Investigation of the Radiative Heating from Aircraft Plume with Particles (입자에 의한 항공기 플룸의 열복사 가열에 관한 연구)

  • Go, Gun-Yung;Yi, Kyung-Joo;Lee, Sung-Nam;Kim, Won-Cheol;Baek, Seung-Wook;Kim, Man-Young
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.40 no.9
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    • pp.737-744
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    • 2012
  • The finite volume method for radiation is applied for the analysis of radiative base heating by SE and PE of the aircraft exhaust plume. The exhaust plume is considered as an absorbing, emitting, and scattering medium, while the base plane is assumed to be cold and black. The radiative properties of non-gray gases are obtained through the WSGGM, and the particle is modelled as spheres. The present method is validated by comparing the results with those of the backward Monte-Carlo method and then the radiative base heating characteristics are analyzed by changing such various parameters as particle concentration, temperature, and scattering phase function. The results show that the radiative heat flux coming into the base plane decreases with altitude and distance, but it increases as the particle temperature increases. The forward scattering of particles increases PE while it decreases SE.

Effects of Input Variables in Radiological Accident Consequence Assessment

  • Han, Moon-Hee;Hwang, Won-Tae;Kim, Eun-Han;Suh, Kyung-Suk;Park, Young-Gil
    • Proceedings of the Korean Nuclear Society Conference
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    • 1998.05b
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    • pp.659-664
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    • 1998
  • The importance of input wariables of real-time accident consequence assessment model has been analyzed. Partial correlation coefficients of input variables related to the plume and the ingestion exposure have been estimated using latino hypercube sampling technique. It is known that wind speed and growth dilution rate are the most important variable in plume and ingestion exposure, respectively.

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On Basic Characteristics of A Pool Fire (Pool fire의 기본적 특성에 관하여)

  • 김명배
    • Fire Science and Engineering
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    • v.11 no.1
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    • pp.55-64
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    • 1997
  • Pool fire는 본격적인 화재연구의 시작과 더불어 그 구조 및 특성에 대한 연구가 지속적으로 수행되어 왔다. Pool fire는 복잡하고 취급하기 어려운 화재의 제문제들을 비교적 간단하게 다룰수 있게 하면서도 현실과 괴리되지 않는 형태를 가지는 가장 기본적인 형태의 화재로, 학문적 측면뿐 아니라 응용측면에서도 매우 유용한 결과 및 단서를 제공하여 왔다. 따라서, 본고에서는 pool fire의 특성을 화염기저(flame base)부근과 플륨(plume)부근으로 나누어 그 동안 발표되었던 연구결과를 정리하고, 화재 시뮬레이션을 위한 zone 모델기법의 가장 중요한 부분의 하나인 연기량 산정과 플륨해석이 어떤 형태로 연결되는 지를 설명하고자 한다.

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Numerical computation of pulsed laser ablation phenomena by thermal mechanisms (열적 메커니즘에 의한 펄스레이저 어블레이션 현상의 수치계산)

  • Oh, Bu-Kuk;Kim, Dong-Sik
    • Proceedings of the KSME Conference
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    • 2003.04a
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    • pp.1572-1577
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    • 2003
  • High-power pulsed laser ablation under atmospheric pressure is studied utilizing numerical and experimental methods with emphasis on recondensation ratio, and the dynamics of the laser induced vapor flow. In the numerical calculation, the temperature pressure, density and vaporization flux on a solid substrate are first obtained by a heat-transfer computation code based on the enthalpy method, and then the plume dynamics is calculated by using a commercial CFD package. To confirm the computation results, the probe beam deflection technique was utilized for measuring the propagation of a laser induced shock wave. Discontinuities of properties and velocity over the Knudsen layer were investigated. Related with the analysis of the jump condition, the effect of the recondesation ratio on the plume dynamics was examined by comparing the pressure, density, and mass fraction of ablated aluminum vapor. To consider the effect of mass transfer between the ablation plume and air, unlike the most previous investigations, the equation of species conservation is simultaneously solved with the Euler equations. Therefore the numerical model computes not only the propagation of the shock front but also the distribution of the aluminum vapor. To our knowledge, this is the first work that employed a commercial CFD code in the calculation of pulsed ablation phenomena.

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Carbon Plume Modeling Assisted by Ar Plasmas (Ar 플라즈마 상태에서 운동하는 탄소 입자 모델링)

  • So, Soon-Youl;Lee, Jin;Chung, Hae-Deok;Yeo, In-Seon
    • Proceedings of the KIEE Conference
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    • 2005.07c
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    • pp.2163-2165
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    • 2005
  • A pulsed laser ablation deposition (PLAD) technique has been used for producing fine particle as well as thin film at relatively low substrate temperatures. However, in order to manufacture and evaluate such materials in detail, motions of plume particles generated by laser ablation have to be understood and interactions between the particles by ablation and gas plasma have to be clarified. Therefore, this paper was focused on the understanding of plume motion in laser ablation assisted by Ar plasma at 50(mTorr). Two-dimensional hybrid model consisting of fluid and particle models was developed and three kinds of plume particles which are carbon atom (C), ion $(C^+)$ and electron were considered in the calculation of particle method It was obtained that ablated $C^+$ was electrically captured in Ar plasmas by strong electric field (E). The difference between motions of the ablated electrons and $C^+$ made E strong and the collisional processes active.

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The Theory of Smoke Movement by a Fire in an Enclosure (밀폐공간에서의 화재에 의한 연기의 유동 이론)

  • 노재성;유홍선
    • Proceedings of the Korea Institute of Fire Science and Engineering Conference
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    • 1996.11a
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    • pp.5-9
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    • 1996
  • In foreign country such as U.S.A and Japan, considerable research has been done regarding the spread of smoke in room of fire involvement by using computer. But, in our country it has not been. So, this paper presents a detailed qualitative description of phenomena which occures during typical fire scenarios through numerical analysis. This research, in the view of field model, is focused on finding out the smoke movement and temperature distribution. And it is planned to analyze governing equation including smoke diffusion equation by numerical analysis with finite volume method and non-staggered grid system. The SIMPLE method for pressure-velocity couple and power-law scheme for convection terms are used. It shows that a plume is formed, hot plume is formed, hot plume gases impinge on the ceiling and they spread across it. then, it eventually reaches the bounding walls of the enclosure. It takes 60s for smoke to fill the enclosure.

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Analysis of Plume Impingement Effect of Lunar Lander (지상시험 모델용 달착륙선 플룸 해석을 통한 추력기간의 간섭 효과 분석)

  • Choi, Ji-Yong;Lee, Jae-Won;Kim, Su-Kyum;Han, Cho-Young;Yu, Myoung-Jong
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2011.11a
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    • pp.254-257
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    • 2011
  • Two types of thrusters(Descent Control Thruster (DCT) for reducing landing speed and Attitude Control Thruster (ACT) for attitude control) are mounted on the propulsion system of Ground test model lunar lander. In this paper, plume impingement effect and ground effect between DCT Modules are analyzed using numerical method when the impact occurred close to the ground.

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A Numerical Experiment on the Dispersion of the Changjiang River Plume

  • Bang, In-Kweon;Lie, Heung-Jae
    • Journal of the korean society of oceanography
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    • v.34 no.4
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    • pp.185-199
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    • 1999
  • With a realistic geography and topography the Princeton Ocean Model is used to study the effects of topography, wind and time-varying Chanajiang (Yangtze) River discharge on the dispersion of the Chanaiiang River plume in the Yellow and East China Seas. The topographic feature of deepening offshore suppresses the offshore expansion of the discharged low salinity water while spreading along the coast is not hindered. Also the spreading of the Chanajiang River plume is very sensitive to wind conditions and the southerly wind is most responsible for the eastward expansion toward the Cheju Island. It is also shown that the influence of the Chanajiang River Diluted Water on the hydrography and circulation of the Yellow Sea including the South Sea of Korea is substantial even in the absence of tide, wind and current.

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A Diagnostic Model for Dye Plume Meandering in Oceanic Waters (해양에서의 염료 플럼의 사행에 대한 모델)

  • Ro, Young-Jae
    • Journal of Korean Society of Coastal and Ocean Engineers
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    • v.2 no.4
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    • pp.200-207
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    • 1990
  • This study is concerned with the meandering of plume axis in oceanic waters. The process is understood that it is a consequence of the differential contribution by the multiple harmonics of local velocity field to variances of center of mass of crossplume as a function of distance from the source point. A diagnostic model is proposed which is aimed to delineate the eddying motions and furthermore the amplified meandering of plumeaxis. From the data base of dye plumes, wave lengths of meandering eddies are estimated to range between 5.5 to 60.3 (m) in coastal surface waters. A numerical simulation is conducted to predict the concentration field of meandering plume.

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