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Flight Investigation from Mach Number 0.8 to 2.0 to Determine Some Effects of Wing-to-tail Distance on the Longitudinal Stability and Control Characteristics of a 60 Degree Delta-wing-canard Missile
Document ID
19930087212
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Brown, Clarence A , Jr
Lundstrom, Reginald R
Date Acquired
August 16, 2013
Publication Date
June 20, 1952
Report/Patent Number
NACA-RM-L52C26
Report Number: NACA-RM-L52C26
Accession Number
93R16502
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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