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Damping in roll of rectangular wings of several aspect ratios and NACA 65A-series airfoil sections of several thickness ratios at transonic and supersonic speeds as determined with rocket-powered models
Document ID
19930090407
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Edmondson, James L
Date Acquired
August 15, 2013
Publication Date
August 24, 1950
Report/Patent Number
NACA-RM-L50E26
Report Number: NACA-RM-L50E26
Accession Number
93R19697
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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