Similarly shaped airfoils to NACA64A318


New! Bulk download of polars in Excel format: NACA64A318.xlsx


Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (1) | 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. NACA63A318
2. GA 37A218
3. NACA65-318 a=0.8
4. GA 35A218
5. NACA65-418
6. GA 40A218
7. NACA65-318 a=0.6
8. NACA65A318
9. NACA65-318
10. GA 40-218
11. NACA64A319
12. NACA64A317
13. NACA65-318 a=0.5
14. NACA63A317
15. NACA65-319 a=0.8
16. NACA63A319
17. NACA65A317
18. GA 37A217
19. NACA65-419
20. NACA64-318 a=0.8
21. GA 35A217