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Effects of leading-edge bluntness and ramp deflection angle on laminar boundary-layer separation in hypersonic flowLeading edge bluntness and ramp deflection angle effects on laminar boundary layer separation in hypersonic flow
Document ID
19660007300
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Townsend, J. C. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
February 1, 1966
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-3290
Report Number: NASA-TN-D-3290
Accession Number
66N16589
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
TWO-DIMENSIONAL FLOW
HYPERSONIC FLOW
FLOW SEPARATION
LEADING EDGE
LAMINAR BOUNDARY LAYER SEPARATION

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