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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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Päätekijät: Razik Benderradji, Hamza Gouidmi, Abdelhadi Beghidja
Aineistotyyppi: Artigo
Kieli:Inglês
Julkaistu: University of El Oued 2020-07-01
Sarja:International Journal of Energetica
Linkit:https://www.ijeca.info/index.php/IJECA/article/view/114
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