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Investigation of effects of ramp span and deflection angle on laminar boundary-layer separation at mach 10.03Ramp span and deflection angle effects on laminar boundary layer separation at hypersonic speed
Document ID
19650014959
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Putnam, L. E. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
May 1, 1965
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-TN-D-2833
Report Number: NASA-TN-D-2833
Accession Number
65N24560
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SEPARATED FLOW
HYPERSONIC SPEED
LAMINAR BOUNDARY LAYER SEPARATION
RAMP

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