Numerical Study of Mixing Enhancement by Shock Waves in Model Scramjet Engine

A numerical study has been conducted to investigate the effect of shock waves on the supersonic hydrogen-air jet flame stabilized in a Mach 2.5 circular cross-section combustor. The numerical model utilizes multispecies Navier-Stokes equations with detailed chemical reaction models and employs a k-w...

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Veröffentlicht in:	AIAA journal 2003-06, Vol.41 (6), p.1074-1080
Hauptverfasser:	Kim, Ji-Ho, Yoon, Youngbin, Jeung, In-Seuck, Huh, Hwanil, Choi, Jeong-Yeol
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerodynamics Airplane engines Applied sciences Energy Energy. Thermal use of fuels Equipments for energy generation and conversion: thermal, electrical, mechanical energy, etc Exact sciences and technology Fluid dynamics Furnaces. Firing chambers. Burners Gaseous fuel burners and combustion chambers
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