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Aerodynamic Characteristics of a Wing with Quarter-chord Line Swept Back 60 Degrees, Aspect Ratio 4, Taper Ratio 0.6, and NACA 65A006 Airfoil Section : Transonic-bump Method
Document ID
19930086059
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
King, Thomas J , Jr
Myers, Boyd C , II
Date Acquired
August 16, 2013
Publication Date
September 6, 1949
Report/Patent Number
NACA-RM-L9G27
Accession Number
93R15349
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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