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Effect of mass injection into a cavity on hypersonic boundary-layer transition.Effect of mass injection into cavity on hypersonic boundary layer transition and on heating downstream
Document ID
19660059444
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Morrisette, E. L.
Date Acquired
August 3, 2013
Publication Date
August 1, 1966
Publication Information
Publication: AIAA JOURNAL
Subject Category
Thermodynamics And Combustion
Accession Number
66A38734
Distribution Limits
Public
Copyright
Other
Keywords
HYPERSONIC HEAT TRANSFER
BOUNDARY LAYER TRANSITION
FLUID INJECTION

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