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Chordwise Pressure Distributions on a 12-foot-span Wing of NACA 66-series Airfoil Sections up to a Mach Number of 0.60
Document ID
19930082337
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Wall, Nancy E
Date Acquired
August 16, 2013
Publication Date
October 1, 1948
Report/Patent Number
NACA-TN-1696
Report Number: NACA-TN-1696
Accession Number
93R11627
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AIRFOILS - NACA 66-SERIES - ORDINATES - LOW-DRAG
WIND TUNNEL TESTS - NACA - HIGH-SPEED (16') WORK CARRIED ON AT LAL
PRESSURE DISTRIBUTION - WINGS

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