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 |
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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 |
| _version_ | 1811276225546551296 |
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| author | Dan PANTAZOPOL |
| author_facet | Dan PANTAZOPOL |
| author_sort | Dan PANTAZOPOL |
| collection | DOAJ |
| 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. |
| first_indexed | 2024-04-12T23:53:49Z |
| format | Article |
| id | doaj.art-8164d385d0b04908a5f9ed37d37adea6 |
| institution | Directory Open Access Journal |
| issn | 2066-8201 2247-4528 |
| language | English |
| last_indexed | 2024-04-12T23:53:49Z |
| publishDate | 2009-09-01 |
| publisher | National Institute for Aerospace Research “Elie Carafoli” - INCAS |
| record_format | Article |
| series | INCAS Bulletin |
| spelling | doaj.art-8164d385d0b04908a5f9ed37d37adea62022-12-22T03:11:37ZengNational 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 |
| spellingShingle | Dan PANTAZOPOL PENETRATION OF A SHOCK WAVE IN A FLAME FRONT INCAS Bulletin |
| title | 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_short | PENETRATION OF A SHOCK WAVE IN A FLAME FRONT |
| title_sort | penetration of a shock wave in a flame front |
| url | http://bulletin.incas.ro/files/dan_pantazopol_v1no1_full.pdf |
| work_keys_str_mv | AT danpantazopol penetrationofashockwaveinaflamefront |