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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