한국추진공학회지 (Journal of the Korean Society of Propulsion Engineers)

  • 제15권6호
  • /
  • Pages.78-90
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  • 2011
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  • 1226-6027(pISSN)
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  • 2288-4548(eISSN)
한국추진공학회 (The Korean Society of Propulsion Engineers)
권호 표지

열-음향학적 불안정 현상의 능동제어를 위한 동역학적 모델링에 관한 현황 분석

A Survey on Dynamical Modeling for Active Control of Thermo-Acoustic Instabilities

  • 나선화 (한국항공대학교 대학원 항공우주 및 기계공학과) ;
  • 고상호 (한국항공대학교 항공우주 및 기계공학과)
  • 투고 : 2011.09.15
  • 심사 : 2011.10.27
  • 발행 : 2011.12.30
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⟨ 이전 논문 다음 논문 ⟩

초록

본 논문에서는 가스터빈 엔진, 로켓 등과 같은 연소시스템에서 발생하는 열음향학적 불안정을 능동적으로 제어하는데 필수적인 동역학적 모델링에 대한 연구 동향을 소개한다. 이를 위하여 1990년대 이후에 진행되었던 관련 연구를 저차의 시스템 모델링 기법을 중심으로 조사하였다. 특히 물리적 원리로부터 모델의 구조를 결정하고 시스템의 입출력 데이터를 기반으로 모델 파라미터를 추정하는 그레이박스 접근방법과 물리적 원리의 적용 없이 시스템 특성을 추정하는 블랙박스 기법을 소개한다. 마지막으로 동 분야에 대한 향후 연구 가능성에 대하여 토의한다.

This paper surveys the recent research activities regarding dynamical modeling of thermo-acoustic instabilities which are fundamental to actively control such phenomena in gas-turbine engines, rockets, and etc. For this, we introduce reduced-order modeling approaches, mainly conducted after 1990s. Particularly, we survey grey-box approaches, which determine the structure of the model based on physical rules and use system's input-output data for estimating parameters of the model. We also introduce black-box approaches using model structures without physics-based interpretation. Finally, we briefly discuss future directions and feasibilities of the research in this field.

키워드

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