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Wind-tunnel Investigation at Mach Numbers from 0.50 to 1.29 of an Unswept Tapered Wing of Aspect Ratio 2.67 with Leading- and Trailing-edge Flaps - Trailing-edge Flaps Deflected
Document ID
19930086395
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Stivers, Louis S , Jr
Malick, Alexander W
Date Acquired
August 16, 2013
Publication Date
December 13, 1950
Report/Patent Number
NACA-RM-A50J09b
Accession Number
93R15685
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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