In wind tunnel investigation, pressure distributions, tuft studies, and boundary layer measurements were obtained for Reynolds number of 5.8 million.
Boundary-layer and stalling characteristics of NACA 63-009 airfoil section
Nat Advisory Committee Aeronautics -- Tech Note
1949
30 pages
Charts
Report
English
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Boundary-layer and stalling characteristics of NACA 64a010 airfoil section
Engineering Index Backfile | 1950
|Boundary-layer and stalling characteristics of NACA 64A006 airfoil section
Engineering Index Backfile | 1949
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