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Some Effects of Aileron Span, Aileron Chord, and Wing Twist on Rolling Effectiveness as Determined by Rocket-powered Model Tests and Theoretical Estimates
Document ID
19930088308
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Strass, H Kurt
Tucker, Warren A
Date Acquired
August 16, 2013
Publication Date
September 14, 1954
Report/Patent Number
NACA-RM-L54G13
Report Number: NACA-RM-L54G13
Accession Number
93R17598
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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