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Some Effects of Sweep and Aspect Ratio on the Transonic Flutter Characteristics of a Series of Thin Cantilever Wings Having a Taper Ratio of 0.6
Document ID
19930088884
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Unangst, John R
Jones, George W , Jr
Date Acquired
August 16, 2013
Publication Date
January 24, 1956
Report/Patent Number
NACA-RM-L55I13a
Report Number: NACA-RM-L55I13a
Accession Number
93R18174
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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