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Tests of NACA 65(216)-420 and 66(218)-420 Airfoils at High Speeds
Document ID
19930092779
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Anderson, Joseph L
Date Acquired
September 6, 2013
Publication Date
April 10, 1944
Report/Patent Number
NACA-WR-A-87
Accession Number
93R22069
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
REYNOLDS NUMBER
AIRFOILS - NACA 65(216)-420 - CHAR , MOMENTS & ORDINATES LOW-DRAG
AIRFOILS - NACA 66(218)-420 - CHAR , MOMENTS & ORDINATES LOW-DRAG
PRESSURE DISTRIBUTION - AIRFOILS - NACA 65(216)-420
AIRFOILS, HIGH-SPEED
AIRFOILS - CHARACTERISTICS - EFFECT OF COMPRESSIBILITY
WIND TUNNEL TESTS - AAL - HIGH-SPEED (16')
PRESSURE DISTRIBUTION - AIRFOILS - NACA 66(218)-420
AIRFOILS - NACA 65,2-420 - CHAR , MOMENTS & ORDINATES LOW-DRAG

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