PENETRATION OF A SHOCK WAVE IN A FLAME FRONT
Journal Title: INCAS BULLETIN - Year 2009, Vol 1, Issue 1
Abstract
The present paper deals with the interactions between a fully supersonic flame front, situated in a supersonic two-dimensional flow of an ideal homogeneous combustible gas mixture, and an incident shock wawe, which is penetrating in the space of the hot burnt gases. A possible configuration, which was named ,,simple penetration” is examined. For the anlysis of the interference phenomena, shock polar and shock-combustion polar are used. At the same time, the paper shows the possibility to produce similar but more complicated configurations, which may contain expansion fans and reflected shock waves.
Authors and Affiliations
PANTAZOPOL Dan
Keywords
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- EP ID EP91948
- DOI 10.13111/2066-8201.2009.1.1.13
- Views 82
- Downloads 0
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