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      LES기반 연소모델과 Helmholtz 방정식을 이용한 LIMOUSINE 버너의 연소불안정 해석

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      https://www.riss.kr/link?id=A103527335

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      다국어 초록 (Multilingual Abstract)

      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.
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      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 combus...

      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.

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      목차 (Table of Contents)

      • ABSTRACT
      • 1. 서론
      • 2. LIMOUSINE 버너
      • 3. 결론
      • References
      • ABSTRACT
      • 1. 서론
      • 2. LIMOUSINE 버너
      • 3. 결론
      • References
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      참고문헌 (Reference)

      1 S. Roux, "Studies of mean and unsteady flow in a swirled combustor using experiments, acoustic analysis, and large eddy simulations" 141 : 40-54, 2005

      2 J. C. Roman, "Non linear Effects in a Lean Partially Premixed Combustor During Limit Cycle" 2012

      3 S. Tufano, "Modelling Flame-generated Noise in a Partially Premixed, Bluff Body Stabilized Model Combustor" 2012

      4 I. Hernandez, "LES and Acoustic Analysis of Thermo-acoustic Instabilities in a Partially Premixed Model Combustor, Combust, spray and flow dynamics for aerospace propuls." 341 : 121-130, 2013

      5 F. Nicoud, "Acoustic modes in combustors with complex impedance and multidimenstional active flame" 45 (45): 426-447, 2007

      6 M. Bauerheim, "A theoretical study of mean azimuthal flow and asymmetry effects on thermos-acoustic modes in annular combustion" 35 : 3219-3227, 2015

      7 Jean-François Parmentier, "A simple analytical model to study and control azimuthal instabilities in annular combustion chambers" 159 : 2374-2387, 2012

      8 김정진, "1D Lumped Method를 이용한 모형 부분 예혼합 가스터빈 연소기의 연소불안정 해석" 한국연소학회 22 (22): 39-45, 2017

      1 S. Roux, "Studies of mean and unsteady flow in a swirled combustor using experiments, acoustic analysis, and large eddy simulations" 141 : 40-54, 2005

      2 J. C. Roman, "Non linear Effects in a Lean Partially Premixed Combustor During Limit Cycle" 2012

      3 S. Tufano, "Modelling Flame-generated Noise in a Partially Premixed, Bluff Body Stabilized Model Combustor" 2012

      4 I. Hernandez, "LES and Acoustic Analysis of Thermo-acoustic Instabilities in a Partially Premixed Model Combustor, Combust, spray and flow dynamics for aerospace propuls." 341 : 121-130, 2013

      5 F. Nicoud, "Acoustic modes in combustors with complex impedance and multidimenstional active flame" 45 (45): 426-447, 2007

      6 M. Bauerheim, "A theoretical study of mean azimuthal flow and asymmetry effects on thermos-acoustic modes in annular combustion" 35 : 3219-3227, 2015

      7 Jean-François Parmentier, "A simple analytical model to study and control azimuthal instabilities in annular combustion chambers" 159 : 2374-2387, 2012

      8 김정진, "1D Lumped Method를 이용한 모형 부분 예혼합 가스터빈 연소기의 연소불안정 해석" 한국연소학회 22 (22): 39-45, 2017

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      학술지 이력

      학술지 이력
      연월일 이력구분 이력상세 등재구분
      2022 평가예정 재인증평가 신청대상 (재인증)
      2019-01-01 평가 등재학술지 유지 (계속평가) KCI등재
      2016-01-01 평가 등재학술지 유지 (계속평가) KCI등재
      2012-01-01 평가 등재학술지 유지 (등재유지) KCI등재
      2009-01-01 평가 등재학술지 선정 (등재후보2차) KCI등재
      2008-01-01 평가 등재후보 1차 PASS (등재후보1차) KCI등재후보
      2007-01-01 평가 등재후보 1차 FAIL (등재후보1차) KCI등재후보
      2005-01-01 평가 등재후보학술지 선정 (신규평가) KCI등재후보
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      학술지 인용정보

      학술지 인용정보
      기준연도 WOS-KCI 통합IF(2년) KCIF(2년) KCIF(3년)
      2016 0.31 0.31 0.29
      KCIF(4년) KCIF(5년) 중심성지수(3년) 즉시성지수
      0.27 0.25 0.632 0.05
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