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Detonation propagation characteristics of H2/O2/AR in multi-angle bifurcation tubes
Affiliation:1. Science and Technology on Scramjet Laboratory, National University of Defense Technology, Changsha, 410073, China;2. Science and Technology on Scramjet Laboratory, China Aerodynamics Research and Development Center, Mianyang, Sichuan, 621000, China;3. Aerodynamics and Flight Mechanics Research Group, University of Southampton, Boldrewood Innovation Campus, Southampton, SO16 7QF, United Kingdom
Abstract:The propagation characteristics of the detonation wave in the bifurcated tube with the angular variation range of 30°–90° are simulated with 25% AR as dilution gas for H2/O2 mixture fuel at chemical equivalence ratio using the solver DCRFoam built on the OpenFOAM platform. The diffraction and reflection phenomena of detonation waves passing through bifurcation tubes with different angles are studied and analyzed. The results show that the distance from regular reflection to Mach reflection increases with the increase of the bifurcation angle so that after one reflection, the detonation forms three reflection forms with the angle of the different bifurcation tubes. After the first reflection, the detonation waves are more likely to induce the formation of transverse waves in the low-angle bifurcation tube. The lowest collision pressure after the detonation collides with the upper wall to form a secondary reflection occurs in the bifurcation tube between 50° and 60°.
Keywords:Bifurcated tube  Shock reflection  Cellular structure  Transverse shocks  AMR"  },{"  #name"  :"  keyword"  ,"  $"  :{"  id"  :"  kwrd0035"  },"  $$"  :[{"  #name"  :"  text"  ,"  _"  :"  adaptive mesh refinement  LS"  },{"  #name"  :"  keyword"  ,"  $"  :{"  id"  :"  kwrd0045"  },"  $$"  :[{"  #name"  :"  text"  ,"  _"  :"  leading shock  TS"  },{"  #name"  :"  keyword"  ,"  $"  :{"  id"  :"  kwrd0055"  },"  $$"  :[{"  #name"  :"  text"  ,"  _"  :"  transverse shock  TPT"  },{"  #name"  :"  keyword"  ,"  $"  :{"  id"  :"  kwrd0065"  },"  $$"  :[{"  #name"  :"  text"  ,"  _"  :"  triple-point trajectory  DS"  },{"  #name"  :"  keyword"  ,"  $"  :{"  id"  :"  kwrd0075"  },"  $$"  :[{"  #name"  :"  text"  ,"  _"  :"  diffracted shock  TD"  },{"  #name"  :"  keyword"  ,"  $"  :{"  id"  :"  kwrd0085"  },"  $$"  :[{"  #name"  :"  text"  ,"  _"  :"  transverse detonation  MS"  },{"  #name"  :"  keyword"  ,"  $"  :{"  id"  :"  kwrd0095"  },"  $$"  :[{"  #name"  :"  text"  ,"  _"  :"  mach stem  DRF"  },{"  #name"  :"  keyword"  ,"  $"  :{"  id"  :"  kwrd0105"  },"  $$"  :[{"  #name"  :"  text"  ,"  _"  :"  decoupled reacting front  RS"  },{"  #name"  :"  keyword"  ,"  $"  :{"  id"  :"  kwrd0115"  },"  $$"  :[{"  #name"  :"  text"  ,"  _"  :"  reflected shock  IS"  },{"  #name"  :"  keyword"  ,"  $"  :{"  id"  :"  kwrd0125"  },"  $$"  :[{"  #name"  :"  text"  ,"  _"  :"  incident shock  IRCR"  },{"  #name"  :"  keyword"  ,"  $"  :{"  id"  :"  kwrd0135"  },"  $$"  :[{"  #name"  :"  text"  ,"  _"  :"  irregular cell region  RCR"  },{"  #name"  :"  keyword"  ,"  $"  :{"  id"  :"  kwrd0145"  },"  $$"  :[{"  #name"  :"  text"  ,"  _"  :"  regular cell region
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