액체로켓엔진 고주파 연소불안정의 예측

Prediction of High Frequency Combustion Instabilities of a Liquid Rocket Engine

  • 윤웅섭 (연세대학교 기계공학부) ;
  • 허환일 (충남대학교 항공우주공학과)
  • 발행 : 2003.09.01

초록

키워드

참고문헌

  1. F. E. C culick & V. Yang , 'Overview of combustion instability in liquid propellant rocket engine', AIAA progress in astronautics and aeronautics Vol. 169, 1995, pp.3-38
  2. J. A. Muss, 'Instability phenomena in Liquid Oxygen/hydrogen propellant rocket engine', AIAA progress in astronautics and aeronautics Vol. 169, 1995, pp. 73-78
  3. J. Hulka & J. J. Hutt, 'Instability phenomena in Liquid Oxygen/hydrogen propellant rocket engine', AIAA progress in astronautics and aeronautics Vol. 169, 1995, pp. 39-72
  4. F. E. C culick & V. Yang , ' Prediction of the stabUity of unsteady motions in solid propellent rocket motor,':nonsteady burning and combustion stability of solid propellant, progress in astronautics and aeronautics, eds. L. Deluca, E. Price and M. Summerfield, 1992
  5. Harrje, D. T. and reardon , F. H, 'Liquid propellant rocket combustion instability,' NASA SP-194, 1972
  6. Wicker, J. M. & Yoon, M. W. & Yang, V.,'Linear and non-linear pressure oscillations in baffled combustion chamber,' journal of sound and Vibration, Vo1.184, 1995, pp. 141-147 https://doi.org/10.1006/jsvi.1995.0309
  7. 이광진, 고영성, 김홍집, 박성진, 정용갑, 문일윤 'Hub and blade 배플이 장착된 연소실의 상온 음향 특성 연구' 한국항공우주학회 추계학술발표회, 2002