Numerical Analysis of Detonation Wave Propagation in Annular Channel

환상 형 도관 내의 데토네이션 파 전파 특성 해석

  • 이수한 (부산대학교 대학원 항공우주공학과) ;
  • 조덕래 (부산대학교 대학원 항공우주공학과) ;
  • 최정열 (부산대학교 항공우주공학과)
  • Published : 2007.11.22

Abstract

Present study examines detonation wave propagation characteristics in annular channel. A normalized value of channel width to the annular radius was considered as a geometric parameter. A parametric study was carried out for a various regimes of detonation waves from weakly unstable to highly unstable detonation waves. Numerical approaches that used in the previous study of numerical requirements of the simulation of detonation wave propagations in 2D and 3D channel were used also for the present study with OpenMP parallization for multi-core SMP machines. The major effect of the curved geometry on the detonation wave propagation seems to be a flow compression effect, regardless of the detonation regimes. The flow compression behind the detonation wave by the curved geometry of the circular channel pushes the detonation wave front and results in the overdriven detonation waves with increased detonation speed beyond the Chapmann-Jouguet speed. This effect gets stronger as the normalized radius smaller, as expected. The effect seems to be negligible beyond the normalized radius of 10.

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