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The Rolling Effectiveness of Wing-tip Ailerons as Determined by Rocket-powered Test Vehicles and Linear Supersonic Theory
Document ID
19930086227
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Sandahl, Carl A
Strass, H Kurt
Piland, Robert O
Date Acquired
August 16, 2013
Publication Date
August 29, 1950
Report/Patent Number
NACA-RM-L50F21
Report Number: NACA-RM-L50F21
Accession Number
93R15517
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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