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Free-flight Tests of 45 Degree Swept Wings of Aspect Ratio 3.15 and Taper Ratio 0.54 to Measure Wing Damping of the First Bending Mode and to Investigate the Possibility of Flutter at Transonic Speeds
Document ID
19930088204
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
O'Kelly, Burke R
Lundstrom, Reginald R
Lauten, William T , Jr
Date Acquired
August 16, 2013
Publication Date
October 12, 1954
Report/Patent Number
NACA-RM-L54C22
Report Number: NACA-RM-L54C22
Accession Number
93R17494
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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