Numerical simulation of transients in the ignition of two-component propellants by intense heat fluxes

A. G. Knyazeva, V. E. Zarko

Результат исследований: Материалы для журналаСтатья

2 Цитирования (Scopus)

Выдержка

An ignition model is developed for quasi-homogeneous propellants consisting of two perfectly mixed compnents which decompose independently in the condensed phase and then react in the gas phase. The model describes the heat propagation in the condensed and gas phases as well as the diffusion of components in the gas phase. The transition processes from ignition to self-sustaining combustion under pulsed irradiation are studied numerically for the simplest case of a monopropellant. It is shown that the critical value of heat flux for stable ignition of monopropellant and the shape of the stable ignition peninsula in the exposure time-heat flux coordinates depend on the extinction criterion.

Язык оригиналаАнглийский
Страницы (с-по)266-269
Число страниц4
ЖурналCombustion, Explosion, and Shock Waves
Том29
Номер выпуска3
DOI
СостояниеОпубликовано - мая 1993

Отпечаток

propellants
Propellants
ignition
Ignition
Heat flux
heat flux
monopropellants
Monopropellants
Gases
Computer simulation
vapor phases
simulation
sustaining
peninsulas
extinction
Irradiation
heat
irradiation
propagation

ASJC Scopus subject areas

  • Materials Science(all)
  • Engineering (miscellaneous)
  • Fuel Technology
  • Energy Engineering and Power Technology
  • Physical and Theoretical Chemistry
  • Fluid Flow and Transfer Processes
  • Chemical Engineering(all)

Цитировать

Numerical simulation of transients in the ignition of two-component propellants by intense heat fluxes. / Knyazeva, A. G.; Zarko, V. E.

В: Combustion, Explosion, and Shock Waves, Том 29, № 3, 05.1993, стр. 266-269.

Результат исследований: Материалы для журналаСтатья

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