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Comparison of flutter calculations using various aerodynamic coefficients with experimental results for some rectangular cantilever wings at Mach number 1.3
Document ID
19930084041
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Nelson, Herbert C
Rainey, Ruby A
Date Acquired
August 16, 2013
Publication Date
November 1, 1954
Report/Patent Number
NACA-TN-3301
Accession Number
93R13331
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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