6A series sections designed to eliminate trailing edge cusp which is characteristic of 6 series sections; theoretical data presented for 6A series basic thickness forms having position of minimum pressure at 30, 50, and 50% chord and with thickness ratios varying from 6 to 15% (published 1949, 20¢).
Theoretical and experimental data for number of NACA 6A-series airfoil sections
Nat Advisory Committee Aeronautics -- Report
1948
21 pages
Report
English
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Theoretical and experimental data for number of NACA 6A-series airfoil sections
Engineering Index Backfile | 1947
|Aerodynamic characteristics of number of modified NACA four-digit-series airfoil sections
Engineering Index Backfile | 1948
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