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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