An Investigation on the Spray Characteristics of Steady/Plused Jet in Crossflow in Model Ramjet Combustor

모델 램제트 연소기 내에서의 정상/가진 수직 분무 특성 연구

  • 김진기 (서울대학교 기계항공공학부 대학원) ;
  • 송진관 (서울대학교 기계항공공학부 대학원) ;
  • 김민기 (서울대학교 기계항공공학부 대학원) ;
  • 윤영빈 (서울대학교 기계항공공학부) ;
  • 황용석 (국방과학연구소)
  • Published : 2008.06.30

Abstract

In this study, spray characteristics research of steady/pulsed injection in crossflow was performed experimentally in the model ramjet combustor. High-speed-camera photography was performed through a visualization window of model combustor, and then, steady and pulsed spray structures were observed and analyzed. Varying influx air temperature and fuel species, we could obtain the trajectory correlation in the steady injection case. In the experiment of pulsed injection, it is found that the pulsed frequency hardly influences spray trajectory. Also, it is found that, in the same injection pressure differential, the trajectory correlation of steady condition can be used for estimating pulsed spray trajectory.

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