MATEC Web Conf.
Volume 115, 2017XXXIII Siberian Thermophysical Seminar (STS-33)
|Number of page(s)||5|
|Section||Chapter 3 Transport processes in physical and chemical transitions, including combustion|
|Published online||10 July 2017|
A mathematical model of metallized solid propellant combustion under the changing pressure
1 Tomsk State University, Department of Physics and Engineering, 634050, Russia, Tomsk, 36 Lenin Ave.
2 Tomsk Politechnical University, Institute of Power Engineering, Department of Theoretical and Industrial Heat Systems Engineering, 634050, Russia, Tomsk, 30 Lenin Ave.
* Corresponding author: firstname.lastname@example.org
This paper presents the mathematical model describing a non-stationary combustion of metallized solid propellant. The model takes into account the heat transfer, the oxidizer decomposition and gasification of the solid propellant, two-phase, dual-velocity, two-temperature reactant flow over the propellant surface. The conditions on the surface perform the conservation of energy and mass fluxes. The model is based on the research works [1, 2]. Our research provides data of the non-stationary burning rate depending on the Al powder dispersion and the pressure drop value.
© The Authors, published by EDP Sciences, 2017
This is an Open Access article distributed under the terms of the Creative Commons Attribution License 4.0, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
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