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The Effects of Centrally Mounted Wing-tip Tanks on the Subsonic Aerodynamic Characteristics of a Wing of Aspect Ratio 10 with 35 Degrees of Sweepback
Document ID
19930086535
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Tinling, Bruce E
Kolk, W Richard
Date Acquired
August 16, 2013
Publication Date
February 21, 1951
Report/Patent Number
NACA-RM-A50K15
Report Number: NACA-RM-A50K15
Accession Number
93R15825
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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