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Damping in roll of straight and 45 degree swept wings of various taper ratios determined at high subsonic, transonic, and supersonic speeds with rocket-powered models
Document ID
19930086866
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Sanders, E Claude, Jr
Date Acquired
September 6, 2013
Publication Date
October 10, 1951
Report/Patent Number
NACA-RM-L51H14
Report Number: NACA-RM-L51H14
Accession Number
93R16156
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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