• Title/Summary/Keyword: Turbulent partially premixed flame

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Combustion of Low Concentration VOC on a Turbulent Partially Premixed Flame (난류 부분예혼합 화염을 이용한 난연성 유증기 처리에 관한 연구)

  • Ahn, Taekook;Park, Sunho;Nam, Younwoo;Lee, Wonnam
    • 한국연소학회:학술대회논문집
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    • 2014.11a
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    • pp.207-210
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    • 2014
  • The potential of combustion treatment of low concentration VOC on a turbulent partially premixed flame has been studied experimentally. The significant decrease in hydrocarbon concentration from the low concentration VOC was observed with a turbulent partially premixed flame. The VOC/inert gas mixture whose fuel concentration is beyond the flammability limit could be treated in this method.

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Modeling of Partially Premixed Turbulent Combustion by Zone-Conditioned Conditional Moment Closure (Zone-conditioned CMC 모델을 이용한 부분예혼합 난류연소 모델링)

  • Lee, Eun-Ju;Kim, Seung H.;Huh, Kang Y.
    • 한국연소학회:학술대회논문집
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    • 2002.06a
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    • pp.41-45
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    • 2002
  • The zone-conditioned CMC equations are derived by taking an unconditional average of the generic conservation equations multiplied by delta and Heaviside functions in terms of mixture fraction and reaction progress variable. The resulting equations are essentially in the same form as the single zone CMC equations except for separate flow fields for burned and unburned gas. The zone-conditioned two-fluid equations are applied to a stagnating turbulent premixed flame brush of Cheng and Shepherd[5l. It is shown that the flame stretch factor is of crucial importance to accurately reproduce the measured mean reaction progress variable and conditional velocities. Further work is in progress for the relationship between surface and volume averages and extension to partially premixed combustion on the basis of a triple flame structure, e. g. in a lifted turbulent diffusion flame.

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Numerical Modeling for Turbulent Partially Premixed Flames (난류 부분 예혼합 화염장에 대한 수치 모델링)

  • Kim, Hoo-Joong;Kim, Yomg-Mo;Ahn, Kook-Young
    • 한국연소학회:학술대회논문집
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    • 2003.05a
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    • pp.191-194
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    • 2003
  • The present study is focused on the subgrid scale combustion model in context with a Large Eddy Simulation. In order to deal with detailed chemical kinetic, the level-set method based on a flamelet model is addressed. In this model, the flame front is treated as an interface, represented by an iso-surface of a scalar field G. This iso-surface is convected by the velocity field and its filtered quantities are include the turbulent burning velocity, which is to be modelled. For modelling the turbulent burning velocity, an equation for the length-scale of the sub-filter flame front fluctuations was developed. The formulations and issues for the turbulent premixed and partially premixed flames are addressed in detail.

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On the Large Eddy Simulation of High Prandtl Number Scalar Transport Using Dynamic Subgrid-Scale Model

  • Na, Yang
    • Journal of Mechanical Science and Technology
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    • v.18 no.1
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    • pp.173-182
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    • 2004
  • The present study has focused on numerical investigation on the flame structure, flame lift-off and stabilization in the partially premixed turbulent lifted jet flames. Since the lifted jet flames have the partially premixed nature in the flow region between nozzle exit and flame base, level set approach is applied to simulate the partially premixed turbulent lifted jet flames for various fuel jet velocities and co-flow velocities. The flame stabilization mechanism and the flame structure near flame base are presented in detail. The predicted lift-off heights are compared with the measured ones.

Numerical Modeling of Turbulent Nonpremixed Lifted Flames

  • Kim, Hoojoong;Kim, Yongmo;Ahn, Kook-Young
    • Journal of Mechanical Science and Technology
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    • v.18 no.1
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    • pp.167-172
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    • 2004
  • The present study has focused on numerical investigation on the flame structure, flame lift-off and stabilization in the partially premixed turbulent lifted jet flames. Since the lifted jet flames have the partially premixed nature in the flow region between nozzle exit and flame base, level set approach is applied to simulate the partially premixed turbulent lifted jet flames for various fuel jet velocities and co-flow velocities. The flame stabilization mechanism and the flame structure near flame base are presented in detail. The predicted lift-off heights are compared with the measured ones.

Utilization and Visualization of Turbulent Partially-premixed Flame for Combustion of Inert-gas-diluted VOC (유증기 연소처리를 위한 난류 부분예혼합화염의 활용 및 유동장 가시화)

  • Ahn, Taekook;Nam, Younwoo;Park, Sunho
    • 한국연소학회:학술대회논문집
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    • 2015.12a
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    • pp.193-196
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    • 2015
  • Combustion of low concentration VOC in inert gas around the flammability limit has been experimentally studied. Streams of nitrogen and propane mixture with various compositions and flow conditions were treated by a turbulent partially-premixed pilot flame. HC and CO contents in exhaust gas measured and the flow patterns were visualized. The results suggested that there exists an optimal mixture velocity range for efficient combustion treatment for each flow condition and composition of the mixture.

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Reduction of Lean VOC Emission by Reforming with a Rotating Arc Plasma and Combustion with a Turbulent Partially-Premixed Flame (난류 부분예혼합화염과 로테이팅 아크 플라즈마를 이용한 난연성 유증기의 연소처리)

  • Ahn, Taekook;Lee, Daehoon;Park, Sunho
    • Journal of the Korean Society of Combustion
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    • v.22 no.1
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    • pp.23-31
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    • 2017
  • Large-scale fuel tanks emit massive amount of hardly-combustible VOC mixtures which are light hydrocarbon species in dilution with nitrogen and carbon dioxide. We have developed a lab-scale burner to combust those VOC mixtures by use of a turbulent partially-premixed flame as a pilot flame. For a higher HC treatment ratio, the mixture gases were reformed by a rotating arc plasma device. The results showed that the nitrogen mole fraction and the injecting speed of the VOC mixture influence on the performance of the burner. It was also found that the size of the pilot flame and the power supplied to the plasma device determine the overall HC treatment ratio and the concentrations of CO and NOx in the exhaust gas.

An Experimental Study on the Lift-off Behavior of Tone-Excited Propane Non-premixed Jet Flames (음향 가진된 프로판 비예혼합 제트 화염의 부상 거동에 대한 실험적 연구)

  • Kim, Seung-Gon;Kim, Kang-Tae;Park, Jeong
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.28 no.5
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    • pp.569-579
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    • 2004
  • The lift-off characteristics of lifted laminar propane jet flames highly diluted with nitrogen are investigated introducing acoustic forcing with a fuel tube resonance frequency. A flame stability curve is obtained according to forcing strength and the nozzle exit velocity for N2 diluted flames. Flame lift-off behavior is globally classified into three regimes; 1) a weakly varying partially premixed behavior caused by a collapsible mixing for large forcing strength, 2) a coexistent behavior of the edge flame and a weakly varying partially premixed behavior for moderate forcing strength, and 3) edge flame or triple flame behavior for small forcing. It is shown that the laminar lifted flame with forcing affects flame lift-off behavior considerably, and is also clarified that the flame characteristic of flame base is well described with the penetration depth of the degree of mixing, ${\gamma}$$\_$$\delta$/. It is also confirmed that the weakly varying partially premixed flame caused by a collapsible mixing fur large forcing strength behaves as that just near flame blow-out in turbulent lift-off flame.

The Effect of Swirl on the Blowout Velocities of Partially Premixed Interacting Flames (스월이 부분예혼합 상호작용화염의 화염날림 유속에 미치는 영향)

  • Lee, Byeong-Jun;Choi, Kwang-Deok
    • Journal of the Korean Society of Combustion
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    • v.14 no.2
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    • pp.26-31
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    • 2009
  • Adding small amounts of air to the fuel is used in many commercial combustors to avoid sooty flame. But partially premixed jet flame has lower blowout velocity, $u_{b.o}$, than nonpremixed one. Increasing blowout limit would be one of the key factors to develope highly intense compact combustion devices. Swirling flow enhances fuel and air mixing and induces a highly turbulent recirculation zone, which helps flame stabilization. It was known that NOx emission decreases with swirl on the proper range of swirl number. And it was shown that the flame interaction in multiple jets also increases $u_{b.o}$ owing to the internal recirculation and reduces NO emission. If the effects of swirl and flame interaction are combined together in partially premixed flame, both $u_{b.o}$ increasement and NOx emission reduction could be achieved. Blowout limits of partially premixed interacting propane flame in the swirling air coflow are investigated experimentally. The results show that the flame is not extinguished up to the experimental limits, 210 m/s, at the swirl number of 0.32 and $X_{F,o}$ = 0.46.

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Combustion Instability Analysis of LIMOUSINE Burner using LES-based Combustion Model and Helmholtz Equation (LES기반 연소모델과 Helmholtz 방정식을 이용한 LIMOUSINE 버너의 연소불안정 해석)

  • Shin, Youngjun;Jeon, Sangtae;Kim, Yongmo
    • Journal of the Korean Society of Combustion
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    • v.22 no.3
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    • pp.41-46
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    • 2017
  • This study has numerically investigated the flame-acoustics interactions in the turbulent partially premixed flame field. In the present approach, in order to analyze the combustion instability, the present approach has employed the LES-based combustion model as well as the Helmholtz solver. Computations are made for the validation case of the partially premixed LIMOUSINE burner. In terms of the FFT data, numerical results are compared with experimental data. Moreover, Helmholtz equation in frequency domain is solved by combining CFD field data including the flight time from a nozzle to the flame zone. Based on numerical results, the detailed discussions are made for the essential features of the combustion instability encountered in the partially premixed burner.