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Effect of Airfoil Section and Tip Tanks on the Aerodynamic Characteristics at High Subsonic Speeds of an Unswept Wing of Aspect Ratio 5.16 and Taper Ratio 0.61
Document ID
19930086008
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
SILVERS H NORMAN
Spreeman, Kenneth P
Date Acquired
August 16, 2013
Publication Date
December 1, 1949
Report/Patent Number
NACA-RM-L9J04
Report Number: NACA-RM-L9J04
Accession Number
93R15298
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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