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Effects of distributed roughness height on aerodynamic characteristics and boundary- layer transition of a wing-body-tail configuration at a mach number of 1.61Effects of three dimensional roughness trips on aerodynamic characteristics and boundary layer transition of wing-body-tail configuration
Document ID
19640012109
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Harris, R. V., Jr. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
June 1, 1964
Subject Category
Aircraft
Report/Patent Number
NASA-TN-D-2334
Report Number: NASA-TN-D-2334
Accession Number
64N22023
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ROUGHNESS
AERODYNAMIC CHARACTERISTICS
BOUNDARY LAYER TRANSITION

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