Similarly shaped airfoils to NACA63(3)-418
New! Bulk download of polars in Excel format: NACA63%283%29-418.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (0) | 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. NACA64(3)-418
3. NACA63-418 a=0.8
4. NACA64-518
5. NACA64-418 a=0.8
6. GA 35-318
7. NACA63-517
8. EPPLER 550
9. NACA63-519
10. NACA63-418
11. NACA63-418 a=0.6
12. GA 37-318
13. NACA63-417 a=0.8
14. EPPLER 552
15. NACA64-517
16. NACA63-419 a=0.8
17. NACA63-618
18. NACA64-519
19. NACA64-418 a=0.6
20. NACA64-418
21. NACA64-618