Similarly shaped airfoils to NACA63-421
New! Bulk download of polars in Excel format: NACA63-421.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (4) | 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
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2. NACA63-420
3. NACA63-320 a=0.8
4. GA 35-220
5. NACA64-420
6. NACA63-320 a=0.6
7. NACA64-320 a=0.8
8. NACA63(4)-421
9. NACA63-320 a=0.5
10. NACA63(4)-221
11. GA 37-220
12. NACA64-320 a=0.6
13. NACA63-320
14. NACA63-420 a=0.8
15. NACA64(4)-421
16. NACA64(4)-221
17. NACA63-520
18. NACA64-420 a=0.8
19. NACA64-320 a=0.5
20. NACA64-520
21. NACA64-320