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Using shock generator for the fuel mixing of the extruded single 4-lobe nozzle at supersonic combustion chamber

Abstract The importance of the fuel injection configuration on the propulsion efficiency of high-speed vehicles is apparent. In this article, the use of an annular extruded 4-lobe nozzle for the injection of fuel jet in a supersonic combustor of a scramjet engine in the existence of a shock generato...

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מידע ביבליוגרפי
Principais autores: As’ad Alizadeh, Dheyaa J. Jasim, Neaman Sohrabi, Mohsen Ahmed, S. Abdul Ameer, Safaa Mohammed Ibrahim, Hasan Khalid Dabis, Ali Adhab Hussein, Abbas J. Sultan
פורמט: Artigo
שפה:Inglês
יצא לאור: Nature Portfolio 2024-03-01
סדרה:Scientific Reports
נושאים:
גישה מקוונת:https://doi.org/10.1038/s41598-024-57103-0
תגים: הוספת תג
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