한국추진공학회지 (Journal of the Korean Society of Propulsion Engineers)

  • 제20권1호
  • /
  • Pages.82-89
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  • 2016
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  • 1226-6027(pISSN)
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  • 2288-4548(eISSN)
한국추진공학회 (The Korean Society of Propulsion Engineers)
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열음향 공진 점화에 대한 연구

Research about Thermoacoustic Resonance Ignition

  • Seo, Seonghyeon (Department of Mechanical Engineering, Hanbat National University) ;
  • Kang, Sang Hun (Department of Aerospace System Engineering, Sejong University) ;
  • Bae, Jong Yeol (Department of Mechanical Engineering, Hanbat National University) ;
  • Lee, Jin Young (Department of Mechanical Engineering, Hanbat National University)
  • 투고 : 2015.12.03
  • 심사 : 2016.01.14
  • 발행 : 2016.02.01
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⟨ 이전 논문 다음 논문 ⟩

초록

초음속 유동의 운동에너지가 열에너지로 바뀌는 열음향 공진 현상을 활용하여 액체로켓엔진의 다중 점화를 위한 점화기 구현에 적용할 수 있다. 본 논문은 이와 같은 열음향 공진 현상의 기본 원리와 이론, 현재까지 진행된 주요 연구결과를 본문에 수록하였다. 열음향 공진 현상에 의한 열발생 특성은 초음속 노즐을 통해 분출되는 유동의 특성과 노즐과 공진관의 형상 그리고 에너지를 전달하는 기체의 종류에 의해 영향 받는다. 이와 같은 열음향 공진 현상을 적용한 액체로켓엔진을 위한 다중 점화기를 구성하는데 있어서 향후 연구 개발이 필요한 부분에 대한 논의를 진행하였다.

The unique phenomenon that jet flow kinetic energy is converted to thermal energy through thermoacoustic resonance can be applied for the multiple ignition of liquid rocket engines. The present article includes the basic principle and theory behind the phenomenon as well as major outstanding, previous research works. The thermoacoustic phenomenon is affected by underexpanded jet flow characteristics from a nozzle, geometries of a nozzle and a resonance tube, and chemical composition of jet flow. The paper concludes with discussion what should be considered as crucial issues for the future research on the development of a multiple ignition system of liquid rocket engines.

키워드

참고문헌

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