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Design method of supercritical hydrocarbon fuel injection for a scramjet

Abstract Both the fuel transfer control scheme and the knowledge of fuel temperature and pressure values before injection are important to a scramjet engine. A measurement method of the fluid temperature suitable for small channel is presented, and a fluid transfer control scheme of the area of inje...

Ausführliche Beschreibung

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Bibliografische Detailangaben
Hauptverfasser: Lei Zhang, Ruoling Zhang, Xiangyi Wang, Jin Jiang
Format: Artigo
Sprache:Inglês
Veröffentlicht: SpringerOpen 2022-10-01
Schriftenreihe:Advances in Aerodynamics
Schlagworte:
Online-Zugang:https://doi.org/10.1186/s42774-022-00123-z
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