Similarly shaped airfoils to NACA64A317


New! Bulk download of polars in Excel format: NACA64A317.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. NACA63A317
2. GA 37A217
3. NACA65-317 a=0.8
4. GA 35A217
5. NACA65-417
6. NACA65-317 a=0.6
7. GA 40A217
8. NACA65A317
9. NACA65-317
10. GA 40-217
11. NACA64A318
12. NACA64A316
13. NACA65-317 a=0.5
14. NACA63A316
15. NREL S822
16. NACA65-318 a=0.8
17. NACA63A318
18. NACA65A316
19. NACA64-317 a=0.8
20. NACA65-418
21. NACA64-417