Similarly shaped airfoils to NACA66-618 a=0.5

1. NACA66-618 a=0.6
2. NACA66-619 a=0.5
3. NACA66-617 a=0.5
4. NACA66-619 a=0.6
5. NACA66-617 a=0.6
6. NACA66-718 a=0.2
7. NACA66-518 a=0.6
8. NACA66-518 a=0.5
9. NACA66-718 a=0.5
10. NACA66-618 a=0.8
11. NACA67-617 a=0.5
12. NACA66A618
13. NACA66-718 a=0.0
14. NACA67-617 a=0.6
15. UAG92 170/SF
16. NACA67-618 a=0.5
17. NACA66-618 a=0.2
18. NACA66-718 a=0.6
19. NACA66-719 a=0.5
20. NACA66-717 a=0.2
21. NACA66-517 a=0.6