Solid-Phase Ignition of a Composite Propellant by a Hot Particle under Free-Convection Heat Sink into the Environment

被引:23
作者
Glushkov, D. O. [1 ]
Kuznetsov, G. V. [1 ]
Strizhak, P. A. [1 ]
机构
[1] Natl Res Tomsk Polytech Univ, Tomsk, Russia
关键词
ignition; convective heat transfer; metallized composite propellant; local energy source; numerical simulation; HIGH-TEMPERATURE; SIMULATION;
D O I
10.1134/S1990793114020146
中图分类号
O64 [物理化学(理论化学)、化学物理学]; O56 [分子物理学、原子物理学];
学科分类号
070203 ; 070304 ; 081704 ; 1406 ;
摘要
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.
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页码:196 / 204
页数:9
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