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Theoretical damping in roll and rolling effectiveness of slender cruciform wings
Document ID
19930083072
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Adams, Gaynor J
Date Acquired
August 29, 2013
Publication Date
January 1, 1951
Report/Patent Number
NACA-TN-2270
Report Number: NACA-TN-2270
Accession Number
93R12362
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
CONTROL, LATERAL
DAMPING DERIVATIVES - STABILITY
MISSILES - COMPONENTS IN COMBINATION
WINGS, COMPLETE - THEORY
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