Turbulent Mixing and Combustion of Multi-Phase Reacting Flows in Ramjet and Ducted Rocket Environment.

Abstract

Experiments with gaseous fuels to establish the base for the multiphase fuel tests were completed for the axisymmetric-coaxial flow fields. Radial and axial profiles of pressure, velocity, species concentration and temperature were determined. Agreement between measured values (velocity and temperature) and computer predictions was, in general, reasonably good. Experiments to determine axial and radial temperature profiles with boron particle-laden fuels were started. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1982
Accession Number
ADA133802

Entities

People

  • K. C. Schadow
  • M. J. Lee

Organizations

  • Naval Air Weapons Station China Lake

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Chemical Reactions
  • Combustion
  • Combustors
  • Ducted Rockets
  • Environment
  • Flow
  • Flow Fields
  • Fuels
  • Gaseous Fuels
  • Gases
  • Hydrodynamics
  • Ignition
  • Measurement
  • Propulsion Systems
  • Rockets
  • Security
  • Turbulent Mixing

Fields of Study

  • Environmental science
  • Physics

Readers

  • Aerodynamics.
  • Combustion science or combustion engineering.
  • Fluid Mechanics and Fluid Dynamics.