PENETRATION OF A SHOCK WAVE IN A FULLY SUPERSONIC FLAME FRONT WITH THE FORMATION OF AN EXPANSION FAN
In a previous paper [3] was treated the ,,simple penetration” of an incident shock wavethrough a fully supersonic flame front in the space of the hot burnt gases, situated in a supersonictwo-dimensional flow of an ideal homogeneous /combustible gas was treated in a previous paper [3].In the present...
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| Formato: | Artigo |
| Idioma: | Inglês |
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National Institute for Aerospace Research “Elie Carafoli” - INCAS
2011-03-01
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| coleção: | INCAS Bulletin |
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| Acesso em linha: | http://bulletin.incas.ro/files/dan_pantazopol_v3is1_full.pdf |
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