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A theoretical investigation of the influence of auxiliary damping in pitch on the dynamic characteristics of a proportionally controlled supersonic canard missile configuration
Document ID
19930086299
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Nelson, Walter C
Passera, Anthony L
Date Acquired
August 16, 2013
Publication Date
August 25, 1950
Report/Patent Number
NACA-RM-L50F30
Report Number: NACA-RM-L50F30
Accession Number
93R15589
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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