Similarly shaped airfoils to NACA63A318


New! Bulk download of polars in Excel format: NACA63A318.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. NACA64A318
2. GA 35A218
3. GA 37A218
4. NACA65-318 a=0.8
5. NACA63A319
6. NACA63A317
7. NACA64A319
8. NACA64-318 a=0.8
9. NACA65-418
10. NACA64-319 a=0.8
11. NACA64-418
12. NACA64-419
13. NACA65-318 a=0.6
14. NACA64A317
15. GA 40A218
16. NACA65-318
17. GA 37-218
18. NACA64-318 a=0.6
19. GA 40-218
20. MS(1)-0317
21. GA 35A217