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2D model for unsteady burning heterogeneous AP/binder solid propellants
Sergey T. Surzhikov
, J. J. Murphy
,
Herman Krier
Mechanical Science and Engineering
Research output
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Contribution to conference
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Paper
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peer-review
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Keyphrases
Solid Propellant
100%
Solid Phase
100%
Binder
100%
2D Model
100%
Gas Phase
66%
Two Dimensional
33%
Chemical Species
33%
Solid Fuel
33%
Chemistry Model
33%
Pyrolysis
33%
Chemical Kinetics
33%
Energy Balance
33%
Kinetic Constants
33%
Species Concentration
33%
Gas Species
33%
Solid Rocket
33%
Burning Rate
33%
Flame Structure
33%
Diffusion Flame
33%
Ammonium Perchlorate
33%
Regression Rate
33%
Solid Oxidizer
33%
Binder Ratio
33%
Reduced Chemistry
33%
Global Reaction
33%
Heat Coupling
33%
Two-dimensional Gas
33%
Heat Exchange Coefficient
33%
Engineering
Two Dimensional
100%
Gas-Phase
100%
Pyrolysis
50%
Parametric Study
50%
Oxidizer
50%
Heat Exchange
50%
Gas Specie
50%
Burning Rate
50%
Solid Fuel
50%
Diffusion Flame
50%
Exchange Coefficient
50%
Material Science
Solid Propellant
100%