Transmission of a Detonation Wave Across a Sudden Expansion with Varying Mixture Composition

Abstract

Detonation waves were examined in axisymmetric and two-dimensional test configurations to determine the limits at which a detonation will successfully initiate and diffract from a small initiator tube into a larger main combustor. Tests were conducted for various initiator-to-main combustor area ratios. Additionally, for each area ratio, the fuel-oxygen initiator mixture was diluted with various nitrogen concentrations attempting to approach the mass fraction of nitrogen in air (79%). Results of the axisymmetric testing showed that with an expansion area ration of 2.0, detonations began to fail to initiate in the initiator section with nitrogen dilution as low as 45%. Although, through constructive interference such as wall reflections and shock-shock interactions, detonation wave initiated in the main combustor for up to 60% nitrogen dilution. Results of the two-dimensional testing showed that for area ratios of 1.33 to 2.67, detonation waves successfully transmitted for all nitrogen dilution cases, including 79%. For an area ratio of 4.0, detonation waves successfully transmitted with 65% nitrogen dilution but failed with 705 nitrogen dilution.

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Document Details

Document Type
Technical Report
Publication Date
Dec 01, 2003
Accession Number
ADA420377

Entities

People

  • Elizabeth J. Touse

Organizations

  • Naval Postgraduate School

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies
  • Materials and Manufacturing Processes
  • Weapons Technologies

DTIC Thesaurus Topics

  • Basic Programming Language
  • Booster Rocket Engines
  • Cameras
  • Chemical Reactions
  • Combustion
  • Combustors
  • Detonation Waves
  • Detonations
  • Engines
  • Geometry
  • Ignition
  • Refractive Index
  • Target Drones
  • Three Dimensional
  • Two Dimensional
  • United States Naval Academy
  • Waves

Readers

  • Analytical Chemistry
  • Combustion Dynamics and Shock Wave Physics.
  • Internal Combustion Engine (ICE) Technology.