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Investigation of a 42.7 Degree Sweptback Wing Model to Determine the Effects of Trailing-edge Thickness on the Aileron Hinge-moment and Flutter Characteristics at Transonic Speeds
Document ID
19930086384
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Thompson, Robert F
Date Acquired
August 16, 2013
Publication Date
December 26, 1950
Report/Patent Number
NACA-RM-L50J06
Report Number: NACA-RM-L50J06
Accession Number
93R15674
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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