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Aerodynamic Characteristics of Tapered Wings Having Aspect Ratios of 4, 6, and 8, Quarter-chord Lines Swept Back 45 Degrees, and NACA 63(sub 1)A012 Airfoil Sections : Transonic-bump Method
Document ID
19930086563
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Polhamus, Edward C
King, Thomas J , Jr
Date Acquired
August 16, 2013
Publication Date
June 13, 1951
Report/Patent Number
NACA-RM-L51C26
Report Number: NACA-RM-L51C26
Accession Number
93R15853
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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