A simplified model for composite propellant burning rate

Keyphrases

• Oxidizer 100%
• Simplified Model 100%
• Composite Propellant 100%
• Propellant Burning Rate 100%
• Condensed Phase 66%
• Gas Phase 66%
• Burning Rate 66%
• Peclet number 66%
• Eigenvalues 33%
• Gas-phase Reactions 33%
• Model Composites 33%
• Particle Size Effect 33%
• Mass Fraction 33%
• Fuel Concentration 33%
• Thermal Decomposition 33%
• Small Interval 33%
• Reaction Sequence 33%
• Pyrolysis 33%
• Reaction Scheme 33%
• Streamwise 33%
• Chemical Kinetics 33%
• Low Activation Energy 33%
• Complex Chemicals 33%
• Heat Release 33%
• Composite Solid 33%
• Eigenvalue Problem 33%
• High Activation Energy 33%
• Propellant 33%
• Combustion Model 33%
• Diffusion Flame 33%
• Asymptotic Analysis 33%
• Phase Decomposition 33%
• Activation Energy Asymptotics 33%
• Composite Solid Propellant 33%
• Non-premixed 33%
• Energy Gases 33%
• Two-phase Reaction 33%
• Heterogeneous Fuel 33%
• Flame Height 33%
• Nitramines 33%

Engineering

• Activation Energy 100%
• Oxidizer 100%
• Gas-Phase 100%
• Burning Rate 100%
• Eigenvalue 66%
• Peclet Number 66%
• Streamwise 33%
• Energetics 33%
• Pyrolysis 33%
• Mass Fraction 33%
• Driving Force 33%
• Fuel Concentration 33%
• Size Effect 33%
• Heat Release 33%
• Reaction Scheme 33%
• Reaction Sequence 33%
• Diffusion Flame 33%
• Phase Reaction 33%
• Obtained Expression 33%

Material Science

• Activation Energy 100%
• Composite Propellant 100%
• Composite Material 100%
• Solid Propellant 33%