Stability of composite solid propellant ignition by a local source of limited energy capacity

Результат исследований: Материалы для журналаСтатьярецензирование

21 Цитирования (Scopus)

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 оригиналаАнглийский
Страницы (с-по)670-675
Число страниц6
ЖурналCombustion, Explosion and Shock Waves
Том50
Номер выпуска6
DOI
СостояниеОпубликовано - 21 ноя 2014

ASJC Scopus subject areas

  • Physics and Astronomy(all)
  • Chemical Engineering(all)
  • Chemistry(all)
  • Energy Engineering and Power Technology
  • Fuel Technology

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