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Effect of large deflection of a canard control and deflections of a wing-tip control on the static-stability and induced-roll characteristics of a cruciform canard missile at a Mach number of 2.01
Document ID
19930087997
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Spearman, M Leroy
Date Acquired
August 16, 2013
Publication Date
December 14, 1953
Report/Patent Number
NACA-RM-L53K03
Report Number: NACA-RM-L53K03
Accession Number
93R17287
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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