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Further investigation of effect of air injection through slots and porous surfaces on flat-plate turbulent skin friction at Mach 3Supersonic flat plate skin friction reduction by air injection into turbulent boundary layer
Document ID
19660011639
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Adcock, J. B. (NASA Langley Research Center Hampton, VA, United States)
Braslow, A. L. (NASA Langley Research Center Hampton, VA, United States)
Mc Ree, D. I. (NASA Langley Research Center Hampton, VA, United States)
Peterson, J. B., Jr. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1966
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-3311
Accession Number
66N20928
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
GAS INJECTION
FLAT PLATE
SUPERSONIC FLOW
FRICTION REDUCTION
TURBULENT BOUNDARY LAYER

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