Passage of SHS wave through a gap: Mathematical modeling


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Stability of combustion wave during its passage through a gaseous gap between two reactive layers was studied by mathematical modeling. The character of transient processes in the gap was explored as a function of thermophysical parameters of the layers, kinetic parameters, and gap width at a predominant role of radiative heat transfer. The passage of combustion wave through the gap was found to be accompanied by the attainment of superadiabatic temperatures within the transition zone. A critical temperature for burning failure at the interface was determined.

作者简介

P. Krishenik

Institute of Structural Macrokinetics and Materials Science

编辑信件的主要联系方式.
Email: petr@ism.ac.ru
俄罗斯联邦, Moscow, 142432

S. Kostin

Institute of Structural Macrokinetics and Materials Science

Email: petr@ism.ac.ru
俄罗斯联邦, Moscow, 142432

S. Rogachev

Institute of Structural Macrokinetics and Materials Science

Email: petr@ism.ac.ru
俄罗斯联邦, Moscow, 142432

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