Increases in camber resulted in large increases in lift and drag divergence Mach numbers at high values of lift coefficient and in augmentation of maximum lift coefficient.
Effects of amount and type of camber on variation with Mach number of aerodynamic characteristics of 10-percent-thick NACA 64A-series airfoil section
Nat Advisory Committee Aeronautics -- Tech Note
1950
66 pages
Charts, tables
Report
Englisch
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