A mathematical model of metallized solid propellant combustion under the changing pressure

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 prop...

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Bibliographic Details
Published in:MATEC Web of conferences Vol. 115. P. 03001 (1-5)
Main Author: Poryazov, Vasily A.
Format: Article
Language:English
Subjects:
Online Access:http://vital.lib.tsu.ru/vital/access/manager/Repository/vtls:000618230
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024 7 |a 10.1051/matecconf/20171150300  |2 doi 
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039 9 |a 201712250801  |c 201712201034  |d VLOAD  |y 201712201009  |z Александр Эльверович Гилязов 
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100 1 |a Poryazov, Vasily A.  |9 562092 
245 1 2 |a A mathematical model of metallized solid propellant combustion under the changing pressure  |c V. Poryazov, A. Y. Krainov, D. A. Krainov 
504 |a Библиогр.: 3 назв. 
520 3 |a 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. 
653 |a математическое моделирование 
653 |a порошок алюминия 
653 |a дисперсия 
653 |a скорость горения 
655 4 |a статьи в журналах  |9 879358 
773 0 |t MATEC Web of conferences  |d 2017  |g Vol. 115. P. 03001 (1-5)  |x 2261-236X 
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856 |y Перейти в каталог НБ ТГУ  |u https://koha.lib.tsu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=496739 
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