A two-dimensional model of composite propellant flame structure and burning rate

Keyphrases

• Ammonium Perchlorate 33%
• Binder Layer 33%
• Burning Rate 100%
• Chemical Kinetics 33%
• Combustion Process 33%
• Composite Propellant 100%
• Composite Propellant Combustion 33%
• Condensed Phase 33%
• Energy Equation 33%
• Experimental Values 33%
• Flame Structure 100%
• Flame Surface 33%
• Free Surface Boundary 33%
• Gas Phase 33%
• Gas-phase Reactions 33%
• High Pressure 33%
• Hydroxyl-terminated Polybutadiene 33%
• Low Pressure 33%
• Merged Flame 33%
• Model Geometry 33%
• Narrow Width 33%
• Oxidizer 66%
• Phase-coupled 33%
• Pressure Sensitivity 33%
• Pressure Variation 33%
• Propellant 33%
• Propellant Formulation 33%
• Pyrolysis 33%
• Sandwich Configuration 33%
• Species Equation 33%
• Steady-state Model 33%
• Surface Geometry 33%
• Two Dimensional 33%
• Two Dimensional Model 100%
• Unique Value 33%

Engineering

• Burning Rate 100%
• Dimensional Model 100%
• Energy Equation 33%
• Experimental Value 33%
• Free Surface 33%
• Gas-Phase 66%
• Leading Edge 33%
• Length Scale 66%
• Model Geometry 33%
• Narrow Width 33%
• Oxidizer 66%
• Phase Reaction 33%
• Pyrolysis 33%
• Specie Equation 33%
• Steady-State Model 33%
• Two Dimensional 100%

Material Science

• Composite Propellant 100%
• Polybutadiene 33%
• Surface (Surface Science) 66%