Abstract
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.
| Original language | English |
|---|---|
| Pages (from-to) | 196-204 |
| Number of pages | 9 |
| Journal | Russian Journal of Physical Chemistry B |
| Volume | 8 |
| Issue number | 2 |
| DOIs | |
| Publication status | Published - 1 Jan 2014 |
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Keywords
- convective heat transfer
- ignition
- local energy source
- metallized composite propellant
- numerical simulation
ASJC Scopus subject areas
- Physical and Theoretical Chemistry
Cite this
Solid-phase ignition of a composite propellant by a hot particle under free-convection heat sink into the environment. / Glushkov, D. O.; Kuznetsov, G. V.; Strizhak, P. A.
In: Russian Journal of Physical Chemistry B, Vol. 8, No. 2, 01.01.2014, p. 196-204.Research output: Contribution to journal › Article
}
TY - JOUR
T1 - Solid-phase ignition of a composite propellant by a hot particle under free-convection heat sink into the environment
AU - Glushkov, D. O.
AU - Kuznetsov, G. V.
AU - Strizhak, P. A.
PY - 2014/1/1
Y1 - 2014/1/1
N2 - 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.
AB - 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.
KW - convective heat transfer
KW - ignition
KW - local energy source
KW - metallized composite propellant
KW - numerical simulation
UR - http://www.scopus.com/inward/record.url?scp=84901047973&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=84901047973&partnerID=8YFLogxK
U2 - 10.1134/S1990793114020146
DO - 10.1134/S1990793114020146
M3 - Article
AN - SCOPUS:84901047973
VL - 8
SP - 196
EP - 204
JO - Russian Journal of Physical Chemistry B
JF - Russian Journal of Physical Chemistry B
SN - 1990-7931
IS - 2
ER -