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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Main Author: Dan PANTAZOPOL
Format: Article
Language:English
Published: National Institute for Aerospace Research “Elie Carafoli” - INCAS 2009-09-01
Series:INCAS Bulletin
Online Access:http://bulletin.incas.ro/files/dan_pantazopol_v1no1_full.pdf
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spelling 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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