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The Rolling Effectiveness of Wing-Tip Ailerons as Determined by Rocket-Powered Test Vehicles and Linear Supersonic Theory
Author:
Sandahl, Carl A.
Additional Authors:
Strass, H. Kurt
Year:
1950
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L50F21
Link:
https://digital.library.unt.edu/ark:/67531/metadc58502/
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