Combustion Mechanisms.

Abstract

The Combustion Mechanism project covered a 6.5 year time period. Its general goal was to use the recently developed laser-based combustion diagnostic probes to learn more about the chemistry and physics occuring in high pressure solid propellant flames. References to published results are included. Keywords: Solid propellant combustion; Combustion diagnostics, Laser-induced fluorescence.

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Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1987
Accession Number
ADA187979

Entities

People

  • R. Timothy Edwards

Tags

DTIC Thesaurus Topics

  • Air Force
  • Air Force Facilities
  • Availability
  • Chemistry
  • Classification
  • Combustion
  • Fluorescence
  • High Pressure
  • Laser Induced Fluorescence
  • Luminescence
  • Molecular Dynamics
  • Physics
  • Propellants
  • Security
  • Solid Propellants
  • Space Systems

Fields of Study

  • Physics

Readers

  • Combustion and Flow Dynamics.
  • Optical Physics and Photonics.
  • Theoretical Analysis.

Technology Areas

  • Directed Energy