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Pressure-distribution Data for the NACA 64(sub 1)-012 and 64(sub 1) A012 Airfoils at High Subsonic Mach Numbers
Document ID
19930085917
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Humphreys, Milton D
Date Acquired
August 16, 2013
Publication Date
May 6, 1949
Report/Patent Number
NACA-RM-L9C18
Accession Number
93R15207
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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