A Study on Flame Dynamics and Combustion Instability Stabilized with a V-gutter Type Flameholder in a model ramjet combustor

V-gutter 형 보염기를 장착한 모델 램제트 연소기의 화염 특성 및 연소 불안정 연구

  • 송진관 (서울대학교 대학원 기계항공공학부) ;
  • 황정재 (서울대학교 대학원 기계항공공학부) ;
  • 송재천 (서울대학교 대학원 기계항공공학부) ;
  • 윤영빈 (서울대학교 기계항공공학부)
  • Published : 2008.11.13

Abstract

The goal of this study is to find flame dynamic behavior using a transverse fuel injection in a model combustor, and is to investigate main causes of unstable combustion in a liquid-fueled combustor. For transverse fuel injection into air cross flow, spray result shows similar tendency with Wu et al.[1998] until spray arrives at flame-holder. However, passing through flame-holder, fuel inflow into recirculation region of flameholder is not sufficient so it makes large difference between shear flame and recirculation flame behind flameholder. In combustion tests, the stable flame shows a kind of shear flames and low peaks of dynamic pressure frequencies. On the other hand, unstable flame shows periodic detached flame in recirculation zone and a strong peak of dynamic pressure frequency. The instability frequency is highly affected by influx air velocity, air temperature, equivalence ratio and wake or vortex shedding frequency behind the flameholder.

Keywords