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Free-flight Investigation, Including Some Effects of Wing Aeroelasticity, of the Rolling Effectiveness of an All-movable Horizontal Tail with Differential Incidence at Mach Numbers from 0.6 to 1.5
Document ID
19930088612
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
English, Roland D
Date Acquired
August 16, 2013
Publication Date
January 25, 1955
Report/Patent Number
NACA-RM-L54K30
Report Number: NACA-RM-L54K30
Accession Number
93R17902
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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