The Effect of the Recombination Shock behind a Backward Step on the Mixing Characteristics of an Inclined Sonic Methane Jet in a Supersonic Crossflow

Authors :: B. Y. C. Chang
D. H. F. Yuan
C. Y. H. Su
A. C. Y. Wen
Source :: 29th International Symposium on Shock Waves 2 ISBN: 9783319168371
Publication Year :: 2015
Publisher :: Springer International Publishing, 2015.
Abstract: The scramjet engines have been extensively studied for use in aircraft and future space transportation systems operating at speeds of about Mach 5 and above. At these high flight velocities, the incoming air is slowed down and maintained supersonic speed within the combustor

Subjects :: Jet (fluid)
symbols.namesake
Materials science
Mach number
Shock (fluid dynamics)
Expansion tunnel
Mixing (process engineering)
symbols
Combustor
Supersonic speed
Scramjet
Mechanics

ISBN :: 978-3-319-16837-1
ISBNs :: 9783319168371
Database :: OpenAIRE
Journal :: 29th International Symposium on Shock Waves 2 ISBN: 9783319168371
Accession number :: edsair.doi...........a2908827a7c4809616097db4730784f6
Full Text :: https://doi.org/10.1007/978-3-319-16838-8_101

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