PENETRATION OF A SHOCK WAVE IN A FLAME FRONT
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 w...
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Format: | Article |
Language: | English |
Published: |
National Institute for Aerospace Research “Elie Carafoli” - INCAS
2009-09-01
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Series: | INCAS Bulletin |
Online Access: | http://bulletin.incas.ro/files/dan_pantazopol_v1no1_full.pdf |