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Preliminary Free-Flight Investigation of the Effect of Airfoil Section on Aileron Rolling Effectiveness at Transonic and Supersonic Speeds
Author:
Sandahl, Carl A.
Year:
1948
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L8B26
Link:
https://digital.library.unt.edu/ark:/67531/metadc57596/
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