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Free-flight Investigation to Determine Some Effects of Tail Damping and Wing-tail Interference on the Rolling Effectiveness of Ailerons and a Spoiler on a Modified-delta Wing at Mach Numbers from 0.6 to 1.5
Document ID
19930089655
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
English, Roland D
Date Acquired
August 16, 2013
Publication Date
May 10, 1957
Report/Patent Number
NACA-RM-L57C13
Report Number: NACA-RM-L57C13
Accession Number
93R18945
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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