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Numerical simulation of ignition in detonation tube with/without obstacles by CE/SE

  • Kong Qian Sun*
  • , Wei Jun Fan
  • , Mao Lin Yang
  • *Corresponding author for this work

Research output: Contribution to journalArticlepeer-review

Abstract

A space-time conservation element and solution element method (CE/SE) was used to simulate the formation and propagation process of two-dimensional detonation with/without obstacles. The detonation mechanisms were analyzed. Influential factors to deflagration to detonation transition (DDT) were evaluated, including the ignition temperature, the tube diameter and the obstacles. Model equation was non-dimensionalized, and the implicit trapezoidal technique was established to handle stiff source term. Results show that the ignition energy is related to the ignition pressure. The higher ignition temperature, the smaller tube diameter or setting obstacles could accelerate DDT process under the condition of small ignition energy. The results offer a reference to study detonation ignition and DDT process.

Original languageEnglish
Pages (from-to)1242-1247
Number of pages6
JournalHangkong Dongli Xuebao/Journal of Aerospace Power
Volume24
Issue number6
StatePublished - Jun 2009

Keywords

  • Deflagration to detonation transition (DDT)
  • Detonation wave
  • Ignition
  • Obstacle
  • Space-time conservation element and solution element method (CE/SE)

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