High-Speed Aerodynamic Characteristics of a Lateral-Control Model 1: NACA 0012-64 Section with 20-Percent-Chord Plain Aileron and 0 Degree and 45 Degrees Sweepback

Author: Anderson, Joseph L.
Year: 1948
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-A8H12
Link: https://digital.library.unt.edu/ark:/67531/metadc57983/

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