Similarly shaped airfoils to NACA64A718
New! Bulk download of polars in Excel format: NACA64A718.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. NACA65-718 a=0.8
3. NACA65A718
4. NACA64A719
5. NACA64A717
6. NACA63A717
7. NACA65-719 a=0.8
8. NACA63A719
9. NACA65A717
10. NACA64-718 a=0.8
11. NACA64A618
12. NACA64-719 a=0.8
13. FX 84-W-175
14. NACA65-618 a=0.8
15. NACA65-717 a=0.8
16. NACA63A618
17. EPPLER 655
18. GA 37A618
19. NACA65-718 a=0.6
20. NACA65A618
21. GA 35A618