Metalized solid propellant combustion under high-speed blowing flow; Journal of Mechanical Science and Technology (JMST); Vol. 34, iss. 5

Metalized solid propellant combustion under high-speed blowing flow; Journal of Mechanical Science and Technology (JMST); Vol. 34, iss. 5

Dades bibliogràfiques
Parent link:	Journal of Mechanical Science and Technology (JMST) Vol. 34, iss. 5.— 2020.— [P. 2245–2253]
Autor corporatiu:	Национальный исследовательский Томский политехнический университет Инженерная школа энергетики Научно-образовательный центр И. Н. Бутакова (НОЦ И. Н. Бутакова)
Altres autors:	Kraynov A. Yu. Aleksey Yurjevich, Poryazov V. A. Vasily Andreevich, Moiseeva K. M. Kseniya Mikhaylovna, Kraynov (Krainov) D. A. Dmitry Alekseevich
Sumari:	Title screen This study presents a mathematical model and a calculation method of the nonstationary combustion rate of metalized solid propellant (nitroglycerin powder with aluminum particle additives) under blowing conditions. The combustion of metalized fuel flat surface under unlimited blowing flow is investigated. The mathematical model describes the erosion effects of solid fuel through boundary layer approximation. The blowing effect is considered in turbulent heat-mass transfer. Results of theoretical and numerical analyses show the influence of aluminum powder additives on the burning rate of solid propellant under blowing flow. This study provides data on the dependence of propellant burning rate on blowing flow speed and dispersion of metal particles in the solid propellant. Режим доступа: по договору с организацией-держателем ресурса
Idioma:	anglès
Publicat:	2020
Matèries:	электронный ресурс труды учёных ТПУ combustion burning rate blowing condition erosion effect metalized solid propellant aluminum particle additive горение металлизированные топлива твердое топливо
Accés en línia:	https://doi.org/10.1007/s12206-020-0446-3
Format:	Electrònic Capítol de llibre
KOHA link:	https://koha.lib.tpu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=664236

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