Combustion Characteristics of Condensed Phase Reactions in Sub-Centimeter Geometries

Abstract

In this work, the combustion characteristics of the exothermic systems Ti/C, Ni/Al, 3Ni/Al and combinations thereof, are examined in small diameter aluminum tubes (3-6 mm ID). Tailoring the overall exothermicity of the reactant system is accomplished by varying the reaction combination, stoichiometry, and the addition of alumina as a diluent. For the combined reactive system, Ti/C-3Ni/Al, it is shown that at 40 wt.% Ti/C content, the failure diameter lies between 3 and 4 mm. While at a Ti/C content of 30 wt.%, complete combustion front propagation is only observed for tube diameters of 6 mm. For the more exothermic system, Ti/C-Ni/Al, studied at a diameter of 4.8 mm, the addition of low levels of alumina as a diluent is shown to drastically alter the combustion front velocity, resulting in extinction with an increase from 2 to 2.5 wt.% addition. The addition of a thermal barrier (Grafoil trademark) for Ti/C-Ni/Al (15/85 wt.%) diluted with 2 wt.% Al2O3, results in an increase in propagation rate and the range of packing densities that complete propagation is observed; the effects of GrafoilTM on the reactive composition Ti/C-3Ni/Al (35/65 wt.%) are not as pronounced.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Jun 10, 2012
Accession Number
ADA566281

Entities

People

  • Anthony P. Shaw
  • Eric J. Miklaszewski
  • Gary Chen
  • Jay C. Poret
  • Lori J. Groven
  • Steven F Son

Organizations

  • United States Army Armament Research, Development and Engineering Center

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Abstracts
  • Aluminum
  • Chemical Reaction Properties
  • Chemical Reactions
  • Combustion
  • Demographic Cohorts
  • Diameters
  • Energy
  • Exothermic Reactions
  • Extinction
  • Geometry
  • Heat Loss
  • Losses
  • Materials
  • Metals
  • Packing Density
  • Stoichiometry

Fields of Study

  • Physics

Readers

  • Combustion science or combustion engineering.
  • Powder metallurgy of Titanium alloys.
  • Reinforced Composite Materials