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

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

التفاصيل البيبلوغرافية
Parent link:Combustion, Explosion, and Shock Waves
Vol. 29, iss. 3.— 1993.— [P. 266-269]
المؤلف الرئيسي: Knyazeva A. G. Anna Georgievna
مؤلفون آخرون: Zarko V. E.
الملخص:Title screen
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.
Режим доступа: по договору с организацией-держателем ресурса
اللغة:الإنجليزية
منشور في: 1993
الموضوعات:
электронный ресурс
труды учёных ТПУ
الوصول للمادة أونلاين:http://link.springer.com/article/10.1007%2FBF00797638
التنسيق: الكتروني فصل الكتاب
KOHA link:https://koha.lib.tpu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=638219

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