Abstract:
The article presents the result of mathematical modeling of oxide formation during burning of agglomerate metal applied to metalized composite solid propellants. The model is based on experimental data obtained by study of evolution of agglomerating particles as well as agglomerates in combustion products flow. The comparison of results of numerical analysis of the model with experimental data led to conclusion about sufficiently high quality of modeling. The principles of using of developed model for description of combustion products evolution in chamber of motor were defined.
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