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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National Institute for Aerospace Research “Elie Carafoli” - INCAS
2009-09-01
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doaj-8164d385d0b04908a5f9ed37d37adea62020-11-25T00:47:54ZengNational Institute for Aerospace Research “Elie Carafoli” - INCASINCAS Bulletin2066-82012247-45282009-09-0111697310.13111/2066-8201.2009.1.1.13PENETRATION OF A SHOCK WAVE IN A FLAME FRONTDan PANTAZOPOLThe 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.http://bulletin.incas.ro/files/dan_pantazopol_v1no1_full.pdf |
collection |
DOAJ |
language |
English |
format |
Article |
sources |
DOAJ |
author |
Dan PANTAZOPOL |
spellingShingle |
Dan PANTAZOPOL PENETRATION OF A SHOCK WAVE IN A FLAME FRONT INCAS Bulletin |
author_facet |
Dan PANTAZOPOL |
author_sort |
Dan PANTAZOPOL |
title |
PENETRATION OF A SHOCK WAVE IN A FLAME FRONT |
title_short |
PENETRATION OF A SHOCK WAVE IN A FLAME FRONT |
title_full |
PENETRATION OF A SHOCK WAVE IN A FLAME FRONT |
title_fullStr |
PENETRATION OF A SHOCK WAVE IN A FLAME FRONT |
title_full_unstemmed |
PENETRATION OF A SHOCK WAVE IN A FLAME FRONT |
title_sort |
penetration of a shock wave in a flame front |
publisher |
National Institute for Aerospace Research “Elie Carafoli” - INCAS |
series |
INCAS Bulletin |
issn |
2066-8201 2247-4528 |
publishDate |
2009-09-01 |
description |
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. |
url |
http://bulletin.incas.ro/files/dan_pantazopol_v1no1_full.pdf |
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