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The Effectiveness at High Speeds of a 20-Percent-Chord Plain Trailing-Edge Flap on the NACA 65-210 Airfoil Section
Author:
Stivers, Louis S., Jr.
Year:
1947
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-SA7A17
Link:
https://digital.library.unt.edu/ark:/67531/metadc65420/
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