• Title/Summary/Keyword: hydrogen jet diffusion flame

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Effects of Shock Waves on the Mixing and the Recirculation Zone of Supersonic Diffusion Flames (초음속 확산화염 내의 혼합과 재순환 영역에 대한 충격파의 영향)

  • Kim, Ji-Ho;Huh, Hwan-Il;Choi, Jeong-Yeol;Yoon, Young-Bin;Jeung, In-Seuck
    • 한국연소학회:학술대회논문집
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    • 1998.10a
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    • pp.123-129
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    • 1998
  • A numerical study has been conducted to investigate the effect of shock waves on the mixing and the recirculation zone of a hydrogen jet diffusion flame in a supersonic combustor. The general trends are compared with the experimental results obtained from the supersonic combustor at the University of Michigan. For the numerical simulation of supersonic diffusion flames, multi-species Navier-Stokes equations and detailed chemistry reaction equations of $H_2$-Air are considered. The $K-{\omega}/k-{\varepsilon}$ blended two equation turbulent model is used. Roe's FDS method and MUSCL method are used for convection fluxes in governing equations. Numerical results show that when slender wedges are mounted at the combustor wall the mixing and the combustion are enhanced and the size of recirculation zone is increased . The flame shape of supersonic flames is different in the flame-tip; it is not closed but open. The flame shape is shown to be greatly affected by shock waves.

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The Characteristics of Unconfined Hydrogen Diffusion Flames in Supersonic Air Flows (초음속 공기 유동장에서의 수소 확산 화염 특성에 대한 연구)

  • 김제흥;심재헌;김지호;윤영빈
    • Journal of the Korean Society of Propulsion Engineers
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    • v.4 no.4
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    • pp.78-86
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    • 2000
  • The objective of this research is to understand the characteristics of a nonpremixed, turbulent, hydrogen jet flame which is stabilized in Mach 1.8 coflowing air flows. In order to investigate the flame structure, flame lengths and fuel trajectories were measured by using direct photography, acetone PLIF, Mie scattering techniques, and numerical simulation. Effect of increasing air velocity was investigated when fuel velocity is fixed. The subsonic flame length was decreased drastically, however the supersonic flame length was increased slowly Then the change of flame blow out characteristics was observed as varying fuel nozzle lip thickness. The flame stability can be increased when fuel nozzle lip thickness was increased, which indicates that the minimum fuel lip thickness ratio is required for the stable supersonic flames. Also, it is found that fuel jet is blocked by high pressure zone and low scattering zone is made. Then the fuel that was moving along the recirculation zone had longer residence time within the supersonic flames, which made partially premixed zone.

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Combustion Characteristics and the Modeling of Ionized Methane for Battery Fires (배터리화재를 모사한 이온화 메탄의 연소특성 및 모델링)

  • Ko, Hyuk-Ju;Lee, Eui-Ju
    • Fire Science and Engineering
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    • v.33 no.1
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    • pp.23-29
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    • 2019
  • Rechargeable battery such as lithium-ion battery has been noticed as a kinds of the energy storage system in the recent energy utilization and widely used actually in various small electronic equipment and electric vehicles. However, many thermal runaway caused battery accidents occurred recently, which still is obstacle for advanced application of lithium ion battery. One of the main differences to general fires is the existence of ionized electrolyte with electron during combustion. Therefore, we simply simulated the ion addition effects of battery fires by introducing an ionized fuel in jet diffusion flames. When the ionized methane through a corona discharge was used as fuel, the overall flame stability and shape such as flame length showed no significant difference from normal methane flame, but NOx and CO emissions measured at the post flame region decreased. The ion addition effect of methane oxidation was also numerically simulated with the modeling of hydrogen addition in the mixture. It was confirmed that the hydrogen addition at a fixed temperature had a similar effects on ionization of methane and hence could be modeled successfully.