Characteristics investigated at Reynolds number of 5,800,000; data on measurements of lift, drag and pitching moment, chordwise distribution of pressure, visual studies of boundary layer flow and surveys of static pressure and velocity distribution within boundary layer.
Boundary-layer and stalling characteristics of NACA 64A006 airfoil section
Nat Advisory Committee Aeronautics -- Tech Note
1949
24 pages
Illus, diagrs, charts
Report
English
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