Similarly shaped airfoils to NACA64-421


Direct link: NACA64-421
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (7) | Similarly shaped airfoils
Plain Flapped Shapes: 25% flap chord | 30% flap chord | 35% flap chord | 40% flap chord
Basic Data: cl vs α | cd vs α | cm vs α | cl/cd vs α | cd vs cl | cl/cd vs cl | cl vs cd | cm vs cl | Curve fits | Lift curve slopes
Data source comparison (Codes, CFD, Wind tunnel)
Compressibility Effects: cl vs α | cd vs α | cm vs α | cl/cd vs α | cd vs cl | cl/cd vs cl | cl vs cd | cm vs cl
Roughness Effects: cl vs α | cd vs α | cm vs α | cl/cd vs α | cd vs cl | cl/cd vs cl | cl vs cd | cm vs cl
Plain Flap Effects: cl,max vs flap deflection: all flap chords | 25% flap chord | 30% flap chord | 35% flap chord | 40% flap chord
Plain Flap Effects: cl vs α for various flap deflections: 25% flap chord | 30% flap chord | 35% flap chord | 40% flap chord
Plain Flap Effects: cm vs α for various flap deflections: 25% flap chord | 30% flap chord | 35% flap chord | 40% flap chord
Plain Flap Effects: cd vs α for various flap deflections: 25% flap chord | 30% flap chord | 35% flap chord | 40% flap chord

Disclaimer: All information presented herein is delivered without guarantee or warranty of any kind. The user assumes the entire risk of use of this information.

1. NACA63-421
2. NACA64-420
3. NACA64-320 a=0.8
4. GA 37-220
5. NACA63-420
6. NACA63-320 a=0.8
7. NACA64-320 a=0.6
8. GA 35-220
9. NACA63A320
10. NACA64(4)-221
11. NACA63-320 a=0.6
12. NACA64-320 a=0.5
13. NACA64-320
14. NACA65-421
15. NACA63(4)-221
16. NACA63-320
17. NACA63-320 a=0.5
18. NACA65-320 a=0.8
19. GA 35A220
20. NACA64-420 a=0.8
21. NACA65-420