Investigation of combustion characteristics in a hydrogen-fueled scramjet combustor

The combustion characteristics of a hydrogen-fueled scramjet combustor were investigated experimentally and numerically. One nonreacting case (case 1), and two different equivalence ratio (ER) reacting cases (cases 2 and 3) were compared. The combustion process of each reacting case was divided into...

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Veröffentlicht in:	Acta astronautica Jg. 186; S. 486 - 495
Hauptverfasser:	Tian, Ye, Shi, Wen, Guo, Mingming, Liu, Yuan, Zhang, Chenlin, Le, Jialing
Format:	Journal Article
Sprache:	Englisch
Veröffentlicht:	Elmsford Elsevier Ltd 01.09.2021 Elsevier BV
Schlagworte:	Combustion Combustion chambers Combustion characteristics Equivalence ratio Hydrogen Hydrogen combustion Ignition Laser induced fluorescence Pressure distribution Scramjet Shear layers Stress concentration Subsonic combustion Supersonic combustion Supersonic combustion ramjet engines Supersonic combustor Wall pressure Supersonic combustor Combustion characteristics Hydrogen Scramjet Ignition
ISSN:	0094-5765, 1879-2030
Online-Zugang:	Volltext
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