Similarly shaped airfoils to NACA67-511 a=0.0

1. NACA67-511 a=0.2
2. NACA67-411 a=0.2
3. NACA66-511 a=0.0
4. NACA67-411 a=0.5
5. NACA66-511 a=0.2
6. NACA66-512 a=0.0
7. NACA67-512 a=0.0
8. NACA67-510 a=0.0
9. NACA66-411 a=0.2
10. NACA67-411 a=0.0
11. NACA67-611 a=0.0
12. NACA67-512 a=0.2
13. NACA66-512 a=0.2
14. NACA67-510 a=0.2
15. NACA67-411 a=0.6
16. NACA67-410 a=0.2
17. NACA66-411 a=0.5
18. NACA66-412 a=0.2
19. NACA67-412 a=0.2
20. NACA66-411 a=0.0
21. NACA67-412 a=0.5