Modeling of Nonlinear Combustion Instability in Solid Propellant Rocket Motors

Abstract

The investigation sought to further our understanding of the physical mechanisms which control the initiation and severity of nonlinear combustion instability in solid propellant rocket motors. It was directed towards understanding those mechanisms which influence the triggering of instabilities

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Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1984
Accession Number
ADA176271

Entities

People

  • Jay N. Levine
  • Joseph D. Baum

Organizations

  • Air Force Research Laboratory

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Boundary Layer
  • Burning Rate
  • Combustion
  • Combustion Chambers
  • Computational Fluid Dynamics
  • Computational Science
  • Computer Programs
  • Differential Equations
  • Energy Transfer
  • Fluid Dynamics
  • Heat Transfer
  • Partial Differential Equations
  • Physics Laboratories
  • Standing Waves
  • Temperature Gradients
  • Wave Propagation
  • Waveforms

Fields of Study

  • Physics

Readers

  • Combustion science or combustion engineering.
  • Control Systems Engineering.
  • Psychological Intervention/Treatment for Stress, Anxiety, PTSD, and Related Emotional and Cognitive Health Symptoms.