Ignition of a Composite Propellant by a Hot Particle under Conditions of a Nonideal Thermal Contact / D. O. Glushkov, G. V. Kuznetsov, P. A. Strizhak

Уровень набора: Russian Journal of Physical Chemistry B, Scientific Journal = 1982-Основной Автор-лицо: Glushkov, D. O., specialist in the field of power engineering, Associate Professor of Tomsk Polytechnic University, Candidate of physical and mathematical sciences, 1988-, Dmitry OlegovichАльтернативный автор-лицо: Kuznetsov, G. V., Specialist in the field of heat power energy, Professor of Tomsk Polytechnic University, Doctor of Physical and Mathematical Sciences, 1949-, Geny Vladimirovich;Strizhak, P. A., Specialist in the field of heat power energy, Doctor of Physical and Mathematical Sciences (DSc), Professor of Tomsk Polytechnic University (TPU), 1985-, Pavel AlexandrovichКоллективный автор (вторичный): Национальный исследовательский Томский политехнический университет (ТПУ), Энергетический институт (ЭНИН), Кафедра теоретической и промышленной теплотехники (ТПТ)Язык: английский.Резюме или реферат: A mathematical modeling of the solidphase ignition of a condensed material by a single diskshaped hot metal particle under conditions of a nonideal thermal contact between the particle and the propellant due to the natural surface roughness of the latter is performed. The ranges of values of the initial temperature of the local energy source and of the parameter characterizing the propellant surface roughness atwhich radiative heat transfer across the gas gap between the propellant and particle significantly (up to 25%)influences the ignition delay time, the main integrated characteristic of the process, are determined fromnumerical simulations..Примечания о наличии в документе библиографии/указателя: [References: p. 636 (21 tit.)].Аудитория: .Тематика: электронный ресурс | труды учёных ТПУ Ресурсы он-лайн:Щелкните здесь для доступа в онлайн
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[References: p. 636 (21 tit.)]

A mathematical modeling of the solidphase ignition of a condensed material by a single diskshaped hot metal particle under conditions of a nonideal thermal contact between the particle and the propellant due to the natural surface roughness of the latter is performed. The ranges of values of the initial temperature of the local energy source and of the parameter characterizing the propellant surface roughness atwhich radiative heat transfer across the gas gap between the propellant and particle significantly (up to 25%)influences the ignition delay time, the main integrated characteristic of the process, are determined fromnumerical simulations.

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