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Drag Measurements of Symmetrical Circular-arc and NACA 65-009 Rectangular Airfoils Having an Aspect Ratio of 2.7 as Determined by Flight Tests at Supersonic Speeds
Document ID
19930085720
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Alexander, Sidney R
Date Acquired
August 16, 2013
Publication Date
March 7, 1947
Report/Patent Number
NACA-RM-L6J14
Report Number: NACA-RM-L6J14
Accession Number
93R15010
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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