Effect of the fluidic injection on the flow of a converging-diverging conical nozzle
The flow in an Over-Expanded Nozzle is subjected to shock waves leading to the unsteady separation of the boundary layer. Free detachment may be followed by a restricted detachment. During the expansion regime in propellant nozzles, several physical phenomena are encountered: supersonic jet, jet sep...
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| Autors principals: | , , |
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| Format: | Artigo |
| Idioma: | Inglês |
| Publicat: |
University of El Oued
2020-07-01
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| Col·lecció: | International Journal of Energetica |
| Accés en línia: | https://www.ijeca.info/index.php/IJECA/article/view/114 |
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