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The effectiveness at high subsonic Mach numbers of a 20-percent-chord plain trailing-edge flap on the NACA 65-210 airfoil section
Document ID
19930083917
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Stivers, Louis S , Jr
Date Acquired
August 16, 2013
Publication Date
March 1, 1954
Report/Patent Number
NACA-TN-3127
Report Number: NACA-TN-3127
Accession Number
93R13207
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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