Effects of Shock Waves on the Mixing and the Recirculation Zone of Supersonic Diffusion Flames
초음속 확산화염 내의 혼합과 재순환 영역에 대한 충격파의 영향
- Kim, Ji-Ho (Department of Aerospace Engineering, Seoul National University) ;
- Huh, Hwan-Il (Department of Aerospace Engineering, Seoul National University) ;
- Choi, Jeong-Yeol (Department of Aerospace Engineering, Pusan National University) ;
- Yoon, Young-Bin (Department of Aerospace Engineering, Seoul National University) ;
- Jeung, In-Seuck (Department of Aerospace Engineering, Seoul National University)
- 김지호 (서울대학교 항공우주공학과) ;
- 허환일 (서울대학교 항공우주공학과) ;
- 최정열 (부산대학교 항공우주공학과) ;
- 윤영빈 (서울대학교 항공우주공학과) ;
- 정인석 (서울대학교 항공우주공학과)
- Published : 1998.10.09
Abstract
A numerical study has been conducted to investigate the effect of shock waves on the mixing and the recirculation zone of a hydrogen jet diffusion flame in a supersonic combustor. The general trends are compared with the experimental results obtained from the supersonic combustor at the University of Michigan. For the numerical simulation of supersonic diffusion flames, multi-species Navier-Stokes equations and detailed chemistry reaction equations of
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