Solid-phase ignition of a composite propellant by a hot particle under free-convection heat sink into the environment

Bibliographic Details
Parent link:Russian Journal of Physical Chemistry B: scientific journal.— , 1982-
Vol. 8, iss. 2.— 2014.— [P. 196-204]
Main Author: Glushkov D. O. Dmitry Olegovich
Corporate Author: Национальный исследовательский Томский политехнический университет Энергетический институт Кафедра теоретической и промышленной теплотехники
Other Authors: Kuznetsov G. V. Geny Vladimirovich, Strizhak P. A. Pavel Alexandrovich
Summary:Title screen
A mathematical model of the solid-phase ignition of a structurally inhomogeneous metallized composite propellant by an incandescent small particle in the form of a cylindrical disk with allowance for free-convection heat sink into the environment is developed. A numerical study of the ignition delay time, the main integral characteristics of the process, is performed. The calculation results are compared to experimental data on the ignition of model propellant compositions based on ammonium perchlorate, butyl rubber, and ASD-4 aluminum powder.
Режим доступа: по договору с организацией-держателем ресурса
Language:English
Published: 2014
Subjects:
Online Access:http://dx.doi.org/10.1134/S1990793114020146
Format: Electronic Book Chapter
KOHA link:https://koha.lib.tpu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=649404

MARC

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200 1 |a Solid-phase ignition of a composite propellant by a hot particle under free-convection heat sink into the environment  |f D. O. Glushkov, G. V. Kuznetsov, P. A. Strizhak 
203 |a Text  |c electronic 
300 |a Title screen 
320 |a [References: p. 203-204 (26 tit.)] 
330 |a A mathematical model of the solid-phase ignition of a structurally inhomogeneous metallized composite propellant by an incandescent small particle in the form of a cylindrical disk with allowance for free-convection heat sink into the environment is developed. A numerical study of the ignition delay time, the main integral characteristics of the process, is performed. The calculation results are compared to experimental data on the ignition of model propellant compositions based on ammonium perchlorate, butyl rubber, and ASD-4 aluminum powder. 
333 |a Режим доступа: по договору с организацией-держателем ресурса 
461 |t Russian Journal of Physical Chemistry B  |o scientific journal  |d 1982- 
463 |t Vol. 8, iss. 2  |v [P. 196-204]  |d 2014 
610 1 |a электронный ресурс 
610 1 |a труды учёных ТПУ 
610 1 |a зажигание 
610 1 |a теплоотдача 
610 1 |a численное моделирование 
610 1 |a источники энергии 
700 1 |a Glushkov  |b D. O.  |c specialist in the field of power engineering  |c Professor, Director of the ISHFVP of the Tomsk Polytechnic University, Doctor of Technical Sciences  |f 1988-  |g Dmitry Olegovich  |3 (RuTPU)RU\TPU\pers\32471  |9 16419 
701 1 |a Kuznetsov  |b G. V.  |c Specialist in the field of heat power energy  |c Professor of Tomsk Polytechnic University, Doctor of Physical and Mathematical Sciences  |f 1949-  |g Geny Vladimirovich  |3 (RuTPU)RU\TPU\pers\31891  |9 15963 
701 1 |a Strizhak  |b P. A.  |c Specialist in the field of heat power energy  |c Doctor of Physical and Mathematical Sciences (DSc), Professor of Tomsk Polytechnic University (TPU)  |f 1985-  |g Pavel Alexandrovich  |3 (RuTPU)RU\TPU\pers\30871  |9 15117 
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