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The Forces and Pressure Distribution at Subsonic Speeds on a Cambered and Twisted Wing Having 45 Degrees of Sweepback and Aspect Ratio of 3 and a Taper Ratio of 0.5
Document ID
19930087199
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Boltz, Frederick W
Kolbe, Carl D
Date Acquired
August 16, 2013
Publication Date
July 18, 1952
Report/Patent Number
NACA-RM-A52D22
Report Number: NACA-RM-A52D22
Accession Number
93R16489
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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