The Effectiveness at High Speeds of a 20-Percent-Chord Plain Trailing-Edge Flap on the NACA 65-210 Airfoil

Author: Stivers, Louis S., Jr.
Year: 1947
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-A7A17
Link: https://digital.library.unt.edu/ark:/67531/metadc64902/

< New search