Numerical Simulation of the Reignition of Detonation by Reflected Shocks

Abstract

We study the diffraction and decay of a detonation wave which occurs when the detonation propagates past an increase in cross-sectional area in a rectangular detonation tube. The computations solve the time-dependent two- dimensional Euler equations using an operator split Flux-Corrected Transport algorithm in an Ar diluted stoichiometric H2/O2 mixture. Previous studies have shown that the initial effect is the decoupling of the reaction front from the shock and the formation of a decaying blast wave or bubble in the larger tube. The detonation may then continue to decay, or be reignited by reflection of the bubble off confining surfaces. In this paper we focus on reignition by shock reflection.

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Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1992
Accession Number
ADA274755

Entities

People

  • D. A. Jones
  • E. S. Oran
  • M. Sichel

Organizations

  • Defence Science and Technology Group

Tags

Communities of Interest

  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Cell Size
  • Cells
  • Cellular Structures
  • Chemical Reactions
  • Combustion
  • Computations
  • Euler Equations
  • Exothermic Reactions
  • Explosives
  • Ignition
  • Materials
  • Military Research
  • Physics
  • Shock Waves
  • Steady State
  • Two Dimensional
  • Waves

Fields of Study

  • Physics

Readers

  • Combustion Dynamics and Shock Wave Physics.
  • Combustion science or combustion engineering.
  • Linear Algebra