Numerical simulation of angular injection of hydrogen fuel in scramjet combustor

Angular injection of hydrogen fuel in a scramjet combustor is explored numerically. Three-dimensional Navier–Stokes equations with turbulence and combustion models are solved using commercial computational fluid dynamics software. Both infinitely fast kinetics and single-step finite rate H2–air kine...

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Veröffentlicht in:	Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering Journal of aerospace engineering, 2012-07, Vol.226 (7), p.861-872
Hauptverfasser:	Chandra Murty, M S R, Chakraborty, D
Format:	Artikel
Sprache:	eng
Schlagworte:	Combustion Computational fluid dynamics Computer simulation Fluid dynamics Hydrogen Hydrogen fuels Mathematical analysis Mathematical models Navier-Stokes equations Partial differential equations Reaction kinetics Scramjets Software Three dimensional Turbulence models
Online-Zugang:	Volltext
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