Similarly shaped airfoils to NACA63A417


New! Bulk download of polars in Excel format: NACA63A417.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
Dynamic plotter New!
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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1. NACA64A417
2. GOE 601
3. GA 35A317
4. NACA65-417 a=0.8
5. NACA64-417 a=0.8
6. GA 37A317
7. NACA65-517
8. NACA63A418
9. NACA63A416
10. NACA64-517
11. NACA64A418
12. NACA64-418 a=0.8
13. NACA64-518
14. NACA64A416
15. NACA65-417 a=0.6
16. NACA64(3)-418
17. LS(1)-0417 (GA(W)-1)
18. NACA64-417 a=0.6
19. NACA65-417
20. NACA65-418 a=0.8
21. GA 40A317