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Aerodynamic Characteristics of a Wing with Quarter-chord Line Swept Back 35 Degrees, Aspect Ratio 4, Taper Ratio 0.6, and NACA 65A006 Airfoil Section : Transonic-bumb Method
Document ID
19930085859
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Sleeman, William C , Jr
Becht, Robert E
Date Acquired
August 16, 2013
Publication Date
April 21, 1949
Report/Patent Number
NACA-RM-L9B25
Report Number: NACA-RM-L9B25
Accession Number
93R15149
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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