Numerical investigation of the flow field behind a shock wave propagation into a carbon-oxygen suspension

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Abstract

The equations governing the flow developed behind a moderately strong shock wave propagating into an oxygen-carbon suspension were developed and solved numerically using the flux corrected transport technique. A comparison is made between two suspensions. In one the carbon particles are assumed to be inert and in the other, the carbon particles combustion is accounted for.
Original languageEnglish
Pages (from-to)684-689
JournalAIP Conference Proceedings
Volume208
DOIs
StatePublished - 1 Jul 1990
Externally publishedYes

Keywords

  • Shock wave interactions and shock effects
  • Chemically reactive flows
  • Shock wave initiated reactions high-pressure chemistry

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