Combustion Instability in Solid Propellant Rockets

Abstract

This report constitutes the principal of a book on combustion stability in solid propellant rockets. The present report contains nine chapters that are each substantially complete except for some editorial, bibliographical and art work in some chapters. Chapters 1 thru 9 include: Introduction to Combustion Instability; Combustion Chamber Processes; Guidance in Missile System and Motor Design; Fundamentals of Propellant Combustion; Analytical Modeling of Combustor Flow; Modeling of Combustion Dynamics; Bulk Mode Oscillations and L* Instability; and Combustor Stability Analysis.

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Document Details

Document Type
Technical Report
Publication Date
Mar 21, 1989
Accession Number
ADA216740

Entities

People

  • Edward W. Price
  • Gary A. Flandro

Organizations

  • Georgia Tech

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Boundary Layer
  • Burning Rate
  • Chemistry
  • Combustion
  • Computational Fluid Dynamics
  • Computational Science
  • Energy Transfer
  • Fluid Dynamics
  • Heat Transfer
  • Materials Laboratories
  • Materials Processing
  • Materials Science
  • Materials Testing
  • Mechanical Properties
  • Physics Laboratories
  • Standing Waves
  • Thermodynamics

Fields of Study

  • Physics

Readers

  • Control Systems Engineering.
  • Library and Information Science
  • Rocket Propulsion.