Аннотация
A numerical simulation of solid-phase ignition of a composite propellant by a single small disk-shaped metal particle heated to a high temperature is performed. In the “heat flux amplitude-ignition delay ” coordinates, an region of stable initiation of combustion of a typical composite solid propellant under local heating by a source of limited energy capacity is selected. The limiting amplitudes of heat fluxes during ignition of the condensed substance under conductive and radiative heating are compared.
Язык оригинала | Английский |
---|---|
Страницы (с-по) | 670-675 |
Число страниц | 6 |
Журнал | Combustion, Explosion and Shock Waves |
Том | 50 |
Номер выпуска | 6 |
DOI | |
Состояние | Опубликовано - 21 ноя 2014 |
ASJC Scopus subject areas
- Physics and Astronomy(all)
- Chemical Engineering(all)
- Chemistry(all)
- Energy Engineering and Power Technology
- Fuel Technology