6A-series airfoil sections designed to eliminate trailing edge cusp characteristic of NACA 6-series sections; data presented for NACA 6A-series basic thickness forms having position of minimum pressure at 30, 40, and 50% chord and with thickness ratios varying from 6 to 15%.
Theoretical and experimental data for number of NACA 6A-series airfoil sections
Nat Advisory Committee Aeronautics -- Tech Note
1947
14 pages
29 Supp Sheets
Report
Englisch
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Theoretical and experimental data for number of NACA 6A-series airfoil sections
Engineering Index Backfile | 1948
|Aerodynamic characteristics of number of modified NACA four-digit-series airfoil sections
Engineering Index Backfile | 1948
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