Effects of injection angle and pressure on mixing performance of fuel injection via various geometries for upstream-fuel-injected scramjets

Published 2016 View Full Article

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Title
Effects of injection angle and pressure on mixing performance of fuel injection via various geometries for upstream-fuel-injected scramjets
Authors
Keywords
Hypersonic airbreathing propulsion, Scramjet engines, Fuel injection, Computational fluid dynamics
Journal
ACTA ASTRONAUTICA
Volume 128, Issue -, Pages 485-498
Publisher
Elsevier BV
Online
2016-08-15
DOI
10.1016/j.actaastro.2016.08.008

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